H-IIA 202 (original) (raw)

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H-IIA 202

Part of H-2

Japanese orbital launch vehicle. Three stage version of H-IIA consisting of 2 x H-II SRB-A + two-stage core vehicle.

Status: Active. First Launch: 2001-08-29. Last Launch: 2018-10-29. Number: 25 . Payload: 10,000 kg (22,000 lb). Thrust: 5,600.00 kN (1,258,900 lbf). Gross mass: 285,000 kg (628,000 lb). Height: 53.00 m (173.00 ft). Diameter: 4.00 m (13.10 ft). Apogee: 40,000 km (24,000 mi).

LEO Payload: 10,000 kg (22,000 lb). Payload: 4,100 kg (9,000 lb) to a GTO.

More at: H-IIA 202.

Family: orbital launch vehicle. Country: Japan. Spacecraft: Daichi-2, Akatsuki, DCAM, DESPATCH, Ginrei, GPM, Horyu, Ikaros, MASCOT, Minerva II, Raijin, Shin'en, Shizuku, SOCRATES, SPROUT, STARS-2, Target Marker, Teikyosat, UNIFORM, Unitec, VEP, ADEOS, KOMPSAT, LRE, FedSat, Mu-Labsat, WEOS Kanta-Kun, IGS, Hayabusa, Cubesat, DS2000, Ibuki, JAXA SDS, Kagayaki, KKS, Kukai, PRISM, SOHLA, SpriteSat. Launch Sites: Tanegashima, Tanegashima Y. Stages: H-2A-1, LE-5B, SRB-A. Agency: Mitsubishi.

2001 August 29 - . 07:00 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

LRE - . Mass: 3,500 kg (7,700 lb). Nation: Japan. Agency: NASDA. Class: Earth. Type: Geodetic satellite. Spacecraft: LRE. USAF Sat Cat: 26898 . COSPAR: 2001-038A. Apogee: 33,306 km (20,695 mi). Perigee: 241 km (149 mi). Inclination: 28.59 deg. Period: 584.29 min.
Launch postponed from february, July 22 and August 25. First launch of the H-2A launch vehicle. A failure after all of the problems with the earlier H-2 version would probably have resulted in cancellation of the program. The Laser Ranging Experiment satellite carried 126 laser retro reflectors and separated from the second stage at 0739 GMT into its operational 'Molniya' type orbit. The eventual goal of H-2A was to launch geosynchronous spacecraft at costs comparable to those of other countries. The LRE remained in a simulated geosynchronous transfer orbit; laser reflections from it would be used to precisely ascertain the orbital injection accuracy of the H-2A.
VEP-2 - . Mass: 3,500 kg (7,700 lb). Nation: Japan. Agency: NASDA. Class: Technology. Type: Navigation technology satellite. Spacecraft: VEP. USAF Sat Cat: 26899 . COSPAR: 2001-038B. Apogee: 35,979 km (22,356 mi). Perigee: 291 km (180 mi). Inclination: 28.60 deg. Period: 636.60 min. Vehicle Evaluation Payload-2 consisted of ballast and monitoring instrumentation that remained attached to the launch vehicle's second stage. It included a Doppler ranging experiment for orbit determination..

2002 December 14 - . 23:04 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Adeos 2 - . Payload: Midori 2. Mass: 3,730 kg (8,220 lb). Nation: Japan. Agency: NASDA. Manufacturer: Mitsubishi. Class: Earth. Type: Earth resources satellite. Spacecraft: Adeos. USAF Sat Cat: 27597 . COSPAR: 2002-056A. Apogee: 806 km (500 mi). Perigee: 804 km (499 mi). Inclination: 98.70 deg. Period: 101.00 min. Environment Monitoring, Aeronomy..
WEOS (Kanta Kun) - . Mass: 50 kg (110 lb). Nation: Japan. Agency: NASDA. Manufacturer: Chiba. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: WEOS. Spacecraft: WEOS. USAF Sat Cat: 27600 . COSPAR: 2002-056D. Apogee: 804 km (499 mi). Perigee: 789 km (490 mi). Inclination: 98.70 deg. Period: 100.80 min. Ecology, Whale Monitoring satellite for Chiba Institute of Technology, Japan..
Mu-Labsat - . Mass: 65 kg (143 lb). Nation: Japan. Agency: NASDA. Class: Technology. Type: Navigation technology satellite. Spacecraft: Mu-Labsat. USAF Sat Cat: 27598 . COSPAR: 2002-056B. Apogee: 806 km (500 mi). Perigee: 793 km (492 mi). Inclination: 98.70 deg. Period: 100.90 min.
Technology. In 2003 the satellite released two tiny subsatellites in an experiment to test an onboard tracking imager for inspector satellites. The RITE (Remote Inspection Technology Experiment) targets are disks about 0.1m in diameter. They were released from Micro-LabSat on 2003 Mar 14 at 0140 UTC and 2003 May 14 at 0150 UTC
FedSat - . Mass: 58 kg (127 lb). Nation: Australia. Agency: CSS. Manufacturer: CRCSS. Class: Communications. Type: Civilian communications satellite. Spacecraft: FedSat. USAF Sat Cat: 27599 . COSPAR: 2002-056C. Apogee: 805 km (500 mi). Perigee: 791 km (491 mi). Inclination: 98.70 deg. Period: 100.80 min.
FedSat contained high-tech communication, space science, navigation and computing equipment and was intended to help bring broadband Internet services to remote parts of Australia. Data from its three-year mission was to be shared between Japan and Australia.

2006 September 11 - . 04:35 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS-3A - . Mass: 850 kg (1,870 lb). Nation: Japan. Agency: JIDF. Manufacturer: Melco. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: IGS. Decay Date: 2016-10-29 . USAF Sat Cat: 29393 . COSPAR: 2006-037A. Apogee: 491 km (305 mi). Perigee: 484 km (300 mi). Inclination: 97.30 deg. Information Gathering Satellite / Optical-2 military surveillance satellite, launched to replace IGS O-1 launched in 2003, which demonstrated technical problems. The first replacement, IGS-O-2, was lost in a launch failure in 2003..

2009 January 23 - . 03:54 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

Ibuki - . Payload: GOSAT. Mass: 1,750 kg (3,850 lb). Nation: Japan. Agency: JAXA. Manufacturer: Mitsubishi. Class: Earth. Type: Earth resources satellite. Spacecraft: Ibuki. USAF Sat Cat: 33492 . COSPAR: 2009-002A. Apogee: 672 km (417 mi). Perigee: 669 km (415 mi). Inclination: 98.00 deg. Period: 98.20 min. Greenhouse Gas Observing Satellite, renamed Ibuki after launch. The satellite carried a TANSO-FTS IR spectrometer and TANSO-CAI cloud and aerosol imager..
PRISM - . Mass: 5.00 kg (11.00 lb). Nation: Japan. Agency: Mitsubishi. Class: Surveillance. Type: Military Radarsat. Spacecraft: PRISM. USAF Sat Cat: 33493 . COSPAR: 2009-002B. Apogee: 641 km (398 mi). Perigee: 614 km (381 mi). Inclination: 98.00 deg. Period: 97.30 min. Remote sensing picosatellite built by the University of Tokyo, with a 10-cm aperture Earth imager on a 1-meter deployable boom..
SDS-1 - . Mass: 100 kg (220 lb). Nation: Japan. Agency: Mitsubishi. Class: Technology. Type: Navigation technology satellite. Spacecraft: JAXA SDS. USAF Sat Cat: 33494 . COSPAR: 2009-002C. Apogee: 668 km (415 mi). Perigee: 663 km (411 mi). Inclination: 98.00 deg. Period: 98.00 min. JAXA Small Demonstration Satellite, a microsatellite with a camera, GPS receiver and sun sensor..
SOHLA-1 - . Mass: 50 kg (110 lb). Nation: Japan. Agency: Mitsubishi. Class: Earth. Type: Weather satellite. Spacecraft: SOHLA. USAF Sat Cat: 33495 . COSPAR: 2009-002D. Apogee: 667 km (414 mi). Perigee: 654 km (406 mi). Inclination: 98.00 deg. Period: 98.00 min. Satellite built by the Space Oriented Higashi-osaka Leading Association, Osaka, carrying a cloud cover imager..
SpriteSat - . Mass: 50 kg (110 lb). Nation: Japan. Agency: Mitsubishi. Class: Earth. Type: Earth resources satellite. Spacecraft: SpriteSat. USAF Sat Cat: 33496 . COSPAR: 2009-002E. Apogee: 668 km (415 mi). Perigee: 658 km (408 mi). Inclination: 98.00 deg. Period: 98.00 min. Microsatellite stabilized by a gravity gradient boom to study atmospheric sprites, built by by Tohoku University, Sendai..
Kagayaki - . Mass: 28 kg (61 lb). Nation: Japan. Agency: Mitsubishi. Class: Technology. Type: Navigation technology satellite. Spacecraft: Kagayaki. USAF Sat Cat: 33497 . COSPAR: 2009-002F. Apogee: 670 km (410 mi). Perigee: 668 km (415 mi). Inclination: 98.00 deg. Period: 98.10 min. Technology satellite built by Sorun Corporation, Tokyo, with several technology payloads..
Kukai - . Mass: 5.00 kg (11.00 lb). Nation: Japan. Agency: Mitsubishi. Class: Technology. Type: Navigation technology satellite. Spacecraft: Kukai. USAF Sat Cat: 33498 . COSPAR: 2009-002G. Apogee: 667 km (414 mi). Perigee: 647 km (402 mi). Inclination: 98.00 deg. Period: 97.90 min. Also named STARS, a Kagawa University picosatellite demonstrating a tethered space robot. It consisted of two tethered box-shaped packages, dubbed Ku and Kai..
KKS 1 - . Mass: 3.00 kg (6.60 lb). Nation: Japan. Agency: Mitsubishi. Class: Surveillance. Type: Military Radarsat. Spacecraft: KKS. USAF Sat Cat: 33499 . COSPAR: 2009-002H. Apogee: 667 km (414 mi). Perigee: 651 km (404 mi). Inclination: 98.00 deg. Period: 97.90 min. Picosatellite built by Kouku-kosen, the Tokyo Metropolitan College of Aeronautical Engineering, carrying an Earth imager..

2009 November 28 - . 01:21 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS O-3 - . Nation: USA. Agency: Mitsubishi. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: IGS. USAF Sat Cat: 36104 . COSPAR: 2009-066A. Information Gathering Satellite, an optical surveillance satellite operated by Japan's Cabinet Satellite Intelligence Center..

2010 May 20 - . 21:58 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

Hayato - . Payload: K-SAT. Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Mitsubishi. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2010-06-28 . USAF Sat Cat: 36573 . COSPAR: 2010-020A. Apogee: 172 km (106 mi). Perigee: 166 km (103 mi). Inclination: 30.00 deg. Period: 87.90 min. 1U cubesat for Kagoshima University, released in parking orbit. Failed..
Waseda-SAT2 - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Mitsubishi. Class: Earth. Type: Earth resources satellite. Spacecraft: Cubesat. Decay Date: 2010-07-12 . USAF Sat Cat: 36574 . COSPAR: 2010-020B. Apogee: 183 km (113 mi). Perigee: 177 km (109 mi). Inclination: 30.00 deg. Period: 88.10 min. 1U cubesat for Waseda University, Tokyo, released in parking orbit. Status unclear..
Negai - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Mitsubishi. Class: Earth. Type: Earth resources satellite. Spacecraft: Cubesat. Decay Date: 2010-06-26 . USAF Sat Cat: 36575 . COSPAR: 2010-020C. Apogee: 190 km (110 mi). Perigee: 176 km (109 mi). Inclination: 30.00 deg. Period: 88.20 min. 1U cubesat for Soka University, Tokyo, released in parking orbit. Successful,.
Akatsuki - . Payload: Planet-C. Mass: 320 kg (700 lb). Nation: Japan. Agency: Mitsubishi. Class: Venus. Type: Venus probe. Spacecraft: Akatsuki. USAF Sat Cat: 36576 . COSPAR: 2010-020D. Venus-orbiting weather satellite with visible, infrared and ultraviolet cameras. Reached Venus on 6 December 2010 but the main engine malfunctioned, preventing the braking burn into Venus orbit. The spacecraft sailed past Venus into solar orbit..
Ikaros - . Mass: 1,000 kg (2,200 lb). Nation: Japan. Agency: Mitsubishi. Class: Technology. Type: Solar sail technology satellite. Spacecraft: Ikaros. USAF Sat Cat: 36577 . COSPAR: 2010-020E.
Solar sail test vehicle. Released in solar orbit 0.72 AU x 1.07 AU x 2.0 deg. Deployed sail by 11 June, and acceleration due to the pressure of the light from the sun was as expected. Flyby of Venus at 80,000 km distance at 07:39 GMT on 8 December 2010 returned images of sail with crescent Vensu in the background.
Unitec-1 - . Payload: Shinen. Mass: 16 kg (35 lb). Nation: Japan. Agency: Mitsubishi. Class: Technology. Type: Technology satellite. Spacecraft: Unitec. USAF Sat Cat: 36578 . COSPAR: 2010-020F. Space qualification of university-built computers. Released in solar orbit 0.72 AU x 1.07 AU x 2.0 deg..

2010 September 11 - . 11:17 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

Michibiki - . Payload: QZS-1. Mass: 4,100 kg (9,000 lb). Nation: Japan. Agency: Mitsubishi. Class: Navigation. Type: Navigation satellite. Spacecraft: DS2000. USAF Sat Cat: 37158 . COSPAR: 2010-045A. Apogee: 38,944 km (24,198 mi). Perigee: 32,632 km (20,276 mi). Inclination: 40.90 deg. Period: 1,436.20 min.
Quasi-Zenith Satellite System; carried an L-band navigation package to augment GPS and a C-band transponder for communications. Placed in an inclined geosynchronous orbit that brings nearly overhead of Japan at peak usage hours, providing a better navigation and communications signal to users which normally would have equatorial geosynchronous satellite and medium-earth-orbit navigation satellite signals interfered with by tall buildings or steep canyons.

2011 September 23 - . 04:36 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS 6A - . Mass: 1,000 kg (2,200 lb). Nation: Japan. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: IGS. USAF Sat Cat: 37813 . COSPAR: 2011-050A. IGS Optical-4 satellite to replenish Japan's military reconnaisance satellite constellation..

2011 December 12 - . 01:21 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS 7A - . Mass: 1,000 kg (2,200 lb). Nation: Japan. Class: Surveillance. Type: Military Radarsat. Spacecraft: IGS. USAF Sat Cat: 37954 . COSPAR: 2011-075A. Apogee: 500 km (310 mi). Perigee: 500 km (310 mi). Inclination: 97.00 deg. Military surveillance radarsat..

2012 May 17 - . 16:39 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Shizuku - . Mass: 1,991 kg (4,389 lb). Nation: Japan. Class: Earth. Type: Climate satellite. Spacecraft: Shizuku. USAF Sat Cat: 38337 . COSPAR: 2012-025A. Apogee: 694 km (431 mi). Perigee: 692 km (429 mi). Inclination: 98.20 deg. Period: 98.60 min. Global Change Observation Mission. Primary instrument was the AMS-4 microwave scanning radiometer..
Arirang-3 - . Payload: Kompsat-3. Mass: 800 kg (1,760 lb). Nation: Korea South. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: T200. Spacecraft: Kompsat. USAF Sat Cat: 38338 . COSPAR: 2012-025B. Apogee: 677 km (420 mi). Perigee: 665 km (413 mi). Inclination: 98.10 deg. Period: 98.20 min. South Korean imaging satellite..
SDS-4 - . Mass: 50 kg (110 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: JAXA SDS. USAF Sat Cat: 38339 . COSPAR: 2012-025C. Apogee: 673 km (418 mi). Perigee: 662 km (411 mi). Inclination: 98.20 deg. Period: 98.10 min. Small Demonstration Satellite; carried four technology experiments including a space-based AIS (ship tracking) payload..
Horyu-2 - . Mass: 7.00 kg (15.40 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: Horyu. USAF Sat Cat: 38340 . COSPAR: 2012-025D. Apogee: 671 km (416 mi). Perigee: 652 km (405 mi). Inclination: 98.20 deg. Period: 98.00 min. Kyushu Institute of Technology satellite to study spacecraft charging effects and test a camera payload for Surrey Satellite (which observed the second stage after payload deployment to support development of improved propellant insulation)..

2013 January 27 - . 04:40 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS 8A - . Payload: JSE Reda-4. Mass: 1,000 kg (2,200 lb). Nation: Japan. Class: Surveillance. Type: Civilian Radarsat. Spacecraft: IGS. USAF Sat Cat: 39061 . COSPAR: 2013-002A. Apogee: 524 km (325 mi). Perigee: 512 km (318 mi). Inclination: 97.50 deg. Period: 94.90 min. IGS military radar satellite 4, with a synthetic aperture radar payload..
IGS 8B (DEMO) - . Payload: Jissho eisei. Mass: 1,000 kg (2,200 lb). Nation: Japan. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: IGS. USAF Sat Cat: 39062 . COSPAR: 2013-002B. Apogee: 524 km (325 mi). Perigee: 512 km (318 mi). Inclination: 97.50 deg. Period: 94.98 min. Demonstration satellite, with a test optical imaging payload..

2014 February 27 - . 18:37 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Ginrei - . Payload: SHINDAISAT. Mass: 33 kg (72 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: Ginrei. Decay Date: 2014-11-24 . USAF Sat Cat: 39572 . COSPAR: 2014-009A. Apogee: 371 km (230 mi). Perigee: 348 km (216 mi). Inclination: 65.01 deg. Period: 91.73 min. Microsatellite from Shinshu University to study use of LED's for long-distance communication..
Hayato-2 - . Payload: ITF 1. Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2014-06-29 . USAF Sat Cat: 39573 . COSPAR: 2014-009B. Apogee: 256 km (159 mi). Perigee: 233 km (144 mi). Inclination: 65.00 deg. Period: 89.40 min. Cubesat from Tsukuba University..
GPM-C - . Mass: 3,850 kg (8,480 lb). Nation: Japan. Class: Earth. Type: Climate Satellite. Spacecraft: GPM. USAF Sat Cat: 39574 . COSPAR: 2014-009C. Apogee: 405 km (251 mi). Perigee: 392 km (243 mi). Inclination: 65.02 deg. Period: 92.53 min.
Joint US-Japanese Global Precipitation Measurement satellite; carried the JAXA/NICT/NEC Toshiba Dual-frequency Precipitation Radar and the GSFC/Ball GPM Microwave Imager. The satellite was built by NASA's Goddard Space Flight Center and registered as a US satellite.
OPUSat - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2014-07-24 . USAF Sat Cat: 39575 . COSPAR: 2014-009D. Apogee: 310 km (190 mi). Perigee: 288 km (178 mi). Inclination: 65.00 deg. Period: 90.50 min. 1U cubesat from Osaka Prefectural University. Technology mission..
Teikyosat-3 - . Mass: 22 kg (48 lb). Nation: Japan. Class: Biology. Type: Biology satellite. Spacecraft: Teikyosat. Decay Date: 2014-10-25 . USAF Sat Cat: 39576 . COSPAR: 2014-009E. Apogee: 359 km (223 mi). Perigee: 338 km (210 mi). Inclination: 65.01 deg. Period: 91.51 min. Microsatellite from Teikyo University..
Invader - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2014-09-02 . USAF Sat Cat: 39577 . COSPAR: 2014-009F. Apogee: 336 km (208 mi). Perigee: 315 km (195 mi). Inclination: 65.01 deg. Period: 91.04 min. Cubesat from Tama Art University..
STARS-2 - . Mass: 22 kg (48 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: STARS-2. Decay Date: 2014-05-18 . USAF Sat Cat: 39578 . COSPAR: 2014-009G. Apogee: 178 km (110 mi). Perigee: 164 km (101 mi). Inclination: 64.97 deg. Period: 87.91 min. Microsatellite from Kagawa University. Composed of two sections and a tether, deployed length 300 metres. Believed to have succeeded based on later orbital decay rate..
Yui - . Payload: K-SAT2. Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Education satellite. Spacecraft: Cubesat. Decay Date: 2014-04-26 . USAF Sat Cat: 39579 . COSPAR: 2014-009H. Apogee: 162 km (100 mi). Perigee: 145 km (90 mi). Inclination: 64.99 deg. Period: 87.56 min. Cubesat from Kagoshima University..

2014 May 24 - . 03:05 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Daichi-2 - . Payload: ALOS 2. Mass: 2,120 kg (4,670 lb). Nation: Japan. Class: Surveillance. Type: Military Radarsat. Spacecraft Bus: Daichi. Spacecraft: Daichi-2. USAF Sat Cat: 39766 . COSPAR: 2014-029A. Apogee: 632 km (392 mi). Perigee: 630 km (390 mi). Inclination: 97.92 deg. Period: 97.33 min. Advanced Land Observing Satellite 2, placed in a noon/midnight sun-synchronous orbit. Carried the PALSAR-2 radar imager with 1 to 3 meter resolution in spotlight mode and 3 to 10 m in high resolution mode..
UNIFORM-1 - . Mass: 50 kg (110 lb). Nation: Japan. Class: Earth. Type: Disaster monitoring satellite. Spacecraft: UNIFORM. USAF Sat Cat: 39767 . COSPAR: 2014-029B. Apogee: 629 km (390 mi). Perigee: 622 km (386 mi). Inclination: 97.87 deg. Period: 97.22 min. Microsatellite for Wakayama University, carrying a 10-12 micron IR microbolometer array for wildfire monitoring..
SOCRATES - . Mass: 50 kg (110 lb). Nation: Japan. Class: Communications. Type: Laser communications satellite. Spacecraft: SOCRATES. USAF Sat Cat: 39768 . COSPAR: 2014-029C. Apogee: 627 km (389 mi). Perigee: 619 km (384 mi). Inclination: 97.87 deg. Period: 97.17 min. Microsatellite for the Japanese communications research lab NICT, with a laser communications experiment..
Raijin-2 - . Payload: RISING 2. Mass: 50 kg (110 lb). Nation: Japan. Class: Science. Type: Science satellite. Spacecraft: Raijin. USAF Sat Cat: 39769 . COSPAR: 2014-029D. Apogee: 630 km (390 mi). Perigee: 626 km (388 mi). Inclination: 97.88 deg. Period: 97.26 min. Microsatellite for Tohoku University mission for studies of lightning with visible and mid-IR imagers and a VLF receiver..
SPROUT - . Mass: 7.00 kg (15.40 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: SPROUT. USAF Sat Cat: 39770 . COSPAR: 2014-029E. Apogee: 627 km (389 mi). Perigee: 615 km (382 mi). Inclination: 97.87 deg. Period: 97.13 min. Microsatellite with a Nihon University experiment to deploy a 1.5m inflatable triangular membrane..

2014 December 3 - . 04:22 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. Launch Pad: Tanegashima Y1. LV Family: H-2. Launch Vehicle: H-IIA 202.

Hayabusa-2 - . Mass: 590 kg (1,300 lb). Nation: Japan. Class: Astronomy. Type: Space probe. Spacecraft: Hayabusa. USAF Sat Cat: 40319 . COSPAR: 2014-076A. Apogee: -50,912 km (-50,912 mi). Perigee: 245 km (152 mi). Inclination: 29.90 deg.
The spacecraft was intended to rendezvous with asteroid 1999 JU3, survey it from orbit, touch down briefly to sample the surface, and return samples to Earth. Launched into a 0.915 AU x 1.089 AU x 6.8 deg solar orbit. Five small, beanbag-like 'target markers' could be ejected onto the surface in advance to help guide the vehicle. Hayabusa-2 also carried three 1 kg class lander/hopper devices, Minerva II-1a, II-1b and II-2, which were to be ejected onto the surface, together with a 10 kg German-built lander called MASCOT. Hayabusa-2 was also to eject a 'Self-Contained Impactor' (SCI) device onto the surface. As the parent spacecraft moved off to the side it would further eject the DCAM-3 camera subsatellite, which would monitor detonation of SCI's high explosive, intended to ram the SCI's body into the asteroid and generate an artificial crater.
Shin'en-2 - . Mass: 15 kg (33 lb). Nation: Japan. Class: Technology. Type: Communications technology satellite. Spacecraft: Shin'en. USAF Sat Cat: 40320 . COSPAR: 2014-076B. Apogee: -50,912 km (-50,912 mi). Perigee: 245 km (152 mi). Inclination: 29.90 deg. Communications payload designed to demonstrate deep space communications with a small spacecraft from a 0.915 AU x 1.089 AU x 6.8 deg solar orbit..
DESPATCH - . Mass: 32 kg (70 lb). Nation: Japan. Class: Technology. Type: Art satellite. Spacecraft: DESPATCH. USAF Sat Cat: 40321 . COSPAR: 2014-076C. Apogee: -50,912 km (-50,912 mi). Perigee: 245 km (152 mi). Inclination: 29.90 deg.
Also known as ArtSat-2; from Tama Art University. The yellowish, tapered-helix assembly was intended mainly as a work of art although it also carries an amateur radio communications payload with a limited range. In a 0.915 AU x 1.089 AU x 6.8 deg solar orbit.
PROCYON - . Mass: 59 kg (130 lb). Nation: Japan. Class: Astronomy. Type: Space probe. USAF Sat Cat: 40322 . COSPAR: 2014-076D. Apogee: -50,912 km (-50,912 mi). Perigee: 245 km (152 mi). Inclination: 29.90 deg.
Small spacecraft experiment to test interplanetary navigation with an ion engine. As of May 2015 the mission plan to perform an Earth swingby followed by flyby of asteroid 2000 DP107 had been abandoned following malfunction of its ion engine. The probe, in solar orbit, continued to make scientific measurements with its ultraviolet camera. Procyon was originally in a 0.9 x 1.1 AU x 6.8 deg solar orbit.
MASCOT - . Nation: Japan. Spacecraft: MASCOT. COSPAR: 2014-076. Attached to Hayabusa-2.
Minerva II-1a - . Nation: Japan. Spacecraft: Minerva II. COSPAR: 2014-076. Attached to Hayabusa-2.
Minerva II-1b - . Nation: Japan. Spacecraft: Minerva II. COSPAR: 2014-076. Attached to Hayabusa-2.
Minerva II-2 - . Nation: Japan. Spacecraft: Minerva II. COSPAR: 2014-076. Attached to Hayabusa-2.
SCI - . Nation: Japan. Spacecraft: Hayabusa. COSPAR: 2014-076. Attached to Hayabusa-2.
DCAM-3 - . Nation: Japan. Spacecraft: DCAM. COSPAR: 2014-076. Attached to Hayabusa-2.
Target Marker 1 - . Nation: Japan. Spacecraft: Target Marker. COSPAR: 2014-076. Attached to Hayabusa-2.
Target Marker 2 - . Nation: Japan. Spacecraft: Target Marker. COSPAR: 2014-076. Attached to Hayabusa-2.
Target Marker 3 - . Nation: Japan. Spacecraft: Target Marker. COSPAR: 2014-076. Attached to Hayabusa-2.
Target Marker 4 - . Nation: Japan. Spacecraft: Target Marker. COSPAR: 2014-076. Attached to Hayabusa-2.
Target Marker 5 - . Nation: Japan. Spacecraft: Target Marker. COSPAR: 2014-076. Attached to Hayabusa-2.

2015 February 1 - . 01:21 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS Radar Spare - . Mass: 1,000 kg (2,200 lb). Nation: Japan. Class: Surveillance. Type: Civilian Radarsat. Spacecraft: IGS. USAF Sat Cat: 40381 . COSPAR: 2015-004A. Apogee: 511 km (317 mi). Perigee: 490 km (300 mi). Inclination: 97.50 deg. The Radar Spare satellite (Reda Yobiki) in the Information Gathering Satellite (Joho Shushu Eisei) series were operated by Japan's Cabinet Satellite Intelligence Center..

2015 March 26 - . 01:21 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS Optical 5 - . Mass: 1,000 kg (2,200 lb). Nation: Japan. Class: Surveillance. Type: Surveillance satellite. Spacecraft: IGS. USAF Sat Cat: 40538 . COSPAR: 2015-015A. Apogee: 515 km (320 mi). Perigee: 511 km (317 mi). Inclination: 97.50 deg. Information Gathering Satellite Optical-5. Military optical surveillance satellite operated by the Japanese government. Sun synchronous orbit; 1015 GMT local time of the descending node..

2016 February 17 - . 08:45 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

Hitomi - . Payload: ASTRO-H. Nation: Japan. Class: Astronomy. Type: X-ray astronomy satellite. USAF Sat Cat: 41337 . COSPAR: 2016-012A. Apogee: 580 km (360 mi). Perigee: 565 km (351 mi). Inclination: 31.00 deg.
ASTRO-H X-ray astronomy observatory rode H2A No. 30 to a low Earth orbit. It carried an array of five X-ray telescopes. Hitomi suffered a major anomaly on Mar 25 while observing the quasar Markarian 205. At 1910 UTC the satellite started tumbling and then at 0140 UTC Mar 26 the spacecraft partly disintegrated. US tracking found eleven debris objects in orbit. During the next scheduled pass at 0740 UTC, JAXA received only a short burst from the radio beacon and nothing more; three more such beacon detections were obtained up to Mar 28, when the spacecraft fell silent. Ground-based optical observations showed that at least two of the debris objects, 2016-012A and 012L, were bright and tumbling several times a minute. 2016-012A was probably the main spacecraft bus. It's possible that 2016-012L was the extensible optical bench with the HXI cameras, or part of the solar panels.
Kinshachi-2 - . Nation: Japan. Class: Surveillance. Type: Surveillance satellite. Spacecraft: ChubuSat. USAF Sat Cat: 41338 . COSPAR: 2016-012B. Apogee: 579 km (359 mi). Perigee: 559 km (347 mi). Inclination: 31.00 deg.
Kinshachi-3 - . Nation: Japan. Class: Science. Type: Science satellite. Spacecraft: ChubuSat. USAF Sat Cat: 41339 . COSPAR: 2016-012C. Apogee: 578 km (359 mi). Perigee: 558 km (346 mi). Inclination: 31.00 deg.
Horyu-4 - . Nation: Japan. Class: Technology. Type: Technology satellite. USAF Sat Cat: 41340 . COSPAR: 2016-012D. Apogee: 578 km (359 mi). Perigee: 557 km (346 mi). Inclination: 31.00 deg.

2016 November 2 - . 06:20 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Himawari 9 - . Nation: Japan. Class: Earth. Type: Weather satellite. Spacecraft: DS2000. USAF Sat Cat: 41836 . COSPAR: 2016-064A. Apogee: 35,857 km (22,280 mi). Perigee: 243 km (150 mi). Inclination: 22.40 deg. Himawari 9 weather satellite was launched to geotransfer orbit by H-IIA-31. By Nov 8 the satellite was on station in GEO at 140.8E..

2017 March 17 - . 01:20 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.

IGS Radar 5 - . Nation: Japan. Class: Surveillance. Type: Military Radarsat. Spacecraft: IGS. USAF Sat Cat: 42072 . COSPAR: 2017-015A. Apogee: 510 km (310 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. See IGS-Radar 5. Japan launched the Joho shushu eisei Reda 5-goki (IGS Radar 5) spy satellite into polar orbit..

2017 June 1 - . 00:16 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Michibiki-2 - . Payload: QZSS 2; QZS-2. Nation: Japan. USAF Sat Cat: 42738 . COSPAR: 2017-028A. Apogee: 38,937 km (24,194 mi). Perigee: 32,634 km (20,277 mi). Inclination: 43.82 deg. Period: 1,436.06 min. See QZS 2 (Michibiki 2). ..

2017 October 9 - . 22:01 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Michibiki-4 - . Payload: QZSS 4; QZS-4. Nation: Japan. USAF Sat Cat: 42965 . COSPAR: 2017-062A. Apogee: 38,943 km (24,198 mi). Perigee: 32,614 km (20,265 mi). Inclination: 40.71 deg. Period: 1,435.68 min. See QZS 4 (Michibiki 4). ..

2017 December 23 - . 01:25 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Shikisai - . Payload: GCOM-C. Nation: Japan. USAF Sat Cat: 43065 . COSPAR: 2017-082A. Apogee: 801 km (497 mi). Perigee: 800 km (490 mi). Inclination: 98.64 deg. Period: 100.89 min. See GCOM-C (Shikisai). ..
Tsubame - . Payload: SLATS. Nation: Japan. USAF Sat Cat: 43066 . COSPAR: 2017-082B. Apogee: 295 km (183 mi). Perigee: 294 km (182 mi). Inclination: 98.31 deg. Period: 90.41 min. See SLATS (Tsubame). ..

2018 February 27 - . 04:33 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

JSE kougaku 6 gouki - . Payload: IGS Optical-6; IGS O-6. Nation: Japan. USAF Sat Cat: 43223 . COSPAR: 2018-021A. See IGS-Optical 6. ..

2018 June 12 - . 04:19 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

JSE reda-6 gouki - . Payload: IGS Radar-6; IGS R-6. Nation: Japan. USAF Sat Cat: 43495 . COSPAR: 2018-052A. See IGS-Radar 6. ..

2018 October 29 - . 04:07 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

Ten-Koh - . Payload: LEO Environments Obs Sat; TENKOU. Nation: Japan. USAF Sat Cat: 43671 . COSPAR: 2018-084A. Apogee: 577 km (358 mi). Perigee: 540 km (330 mi). Inclination: 97.82 deg. Period: 95.83 min. See Ten-Koh. ..
Ibuki 2 - . Payload: GOSAT 2. Nation: Japan. USAF Sat Cat: 43672 . COSPAR: 2018-084B. Apogee: 617 km (383 mi). Perigee: 615 km (382 mi). Inclination: 97.83 deg. Period: 97.02 min. See GOSAT 2 (Ibuki 2). ..
KhalifaSat - . Nation: UAE. USAF Sat Cat: 43676 . COSPAR: 2018-084F. Apogee: 613 km (380 mi). Perigee: 591 km (367 mi). Inclination: 97.83 deg. Period: 96.73 min. See KhalifaSat. ..
Diwata-2B - . Nation: Philippines. USAF Sat Cat: 43678 . COSPAR: 2018-084H. Apogee: 601 km (373 mi). Perigee: 586 km (364 mi). Inclination: 97.84 deg. Period: 96.55 min. See Diwata 2B. ..
AUTCube-2 - . Nation: Japan. USAF Sat Cat: 43679 . COSPAR: 2018-084J. Apogee: 599 km (372 mi). Perigee: 585 km (363 mi). Inclination: 97.84 deg. Period: 96.52 min. See AUTcube 2 (Gamacube). ..
Aoi - . Payload: STARS-AO. Nation: TBD. USAF Sat Cat: 43681 . COSPAR: 2018-084K. Apogee: 600 km (370 mi). Perigee: 586 km (364 mi). Inclination: 97.84 deg. Period: 96.54 min. See STARS-AO (Aoi). ..

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