LEOStar-2 (original) (raw)

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LEOStar-2 FURTHER INFORMATION ON THIS TOPIC AT OUR PARTNER SITE

?Civil or defense satellite bus for use in ?LEO orbit and launch by ?Pegasus or Minotaur I, IV or C. Lifetime ??1-5 years and delivery possible ?16-36 months after receipt of order. Electrical system solar cells, average power 750W

Status: Operational 2014. First Launch: 2014-04-30. Last Launch: 2014-07-02. Number: 2 . Gross mass: 500 kg (1,100 lb).

More at: LEOStar-2.

Subtopics

OrbView 4 Earth observing satellite built by Orbital Sciences Corporation (OSC) for OrbImage, USA. Launched 2001. Used the LEOStar-2 bus.

	SORCE American solar satellite. Earth science satellite built by Orbital Sciences Corporation (OSC) for NASA, USA. Launched 2003. Used the LEOStar-2 bus.

	Galex American ultraviolet astronomy satellite. The Galaxy Evolution Explorer (GALEX) was an orbiting space telescope that was to observe galaxies in ultraviolet wavelengths. Astronomy, UV satellite built by Orbital Sciences Corporation (OSC) for NASA, USA. Launched 2003. Used the LEOStar-2 bus.

OCO Orbiting Carbon Observatory. Launched 2009.02.24, Earth Science satellite built by Orbital Sciences Corporation (OSC) for NASA, USA. Launched 2009 - 2014. Used the LEOStar-2 bus.

OCO 3 Earth Science satellite operated by NASA, USA.

Family: Surveillance. Country: USA. Launch Vehicles: Thor, Delta 7320-10C, Vega. Launch Sites: Vandenberg SLC2W, Kourou ELV. Bibliography: 12758.

2003 January 25 - . 20:13 GMT - . Launch Site: Cape Canaveral. Launch Complex: Mayport DZ. Launch Pad: 29.0 N x 78.5 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL.

SORCE - . Payload: Solstice/SAVE. Mass: 268 kg (590 lb). Nation: USA. Agency: NASA. Manufacturer: OSC. Class: Astronomy. Type: Solar satellite. Spacecraft Bus: LEOStar-2. Spacecraft: SORCE. USAF Sat Cat: 27651 . COSPAR: 2003-004A. Apogee: 657 km (408 mi). Perigee: 617 km (384 mi). Inclination: 39.99 deg. Period: 97.31 min. Solar irradiance monitoring, climatology mission. Launch delayed from December 1 and 13, 2002. Air dropped in Mayport DZ..

2003 April 28 - . 12:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Mayport DZ. Launch Pad: 29.0 N x 78.5 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL.

Galex - . Mass: 280 kg (610 lb). Nation: USA. Agency: NASA. Manufacturer: OSC. Class: Astronomy. Type: Ultraviolet astronomy satellite. Spacecraft Bus: LEOStar-2. Spacecraft: Galex. Duration: 3,710.00 days. USAF Sat Cat: 27783 . COSPAR: 2003-017A. Apogee: 699 km (434 mi). Perigee: 694 km (431 mi). Inclination: 29.00 deg. Period: 98.70 min.
Ultraviolet space telescope. Much delayed launch (from January 19, May 19, July 16, 21 and 30, August 14 and October 17, 2002; January 27, March 25 and 30, April 15 and 26 2003). It was finally switched off on 28 June 2013, following an extra tenth year of observing funded by Caltech. Air dropped in Mayport DZ.

2014 April 30 - . 01:38 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELV. Launch Vehicle: Vega.

KazEOSat-1 - . Mass: 830 kg (1,820 lb). Nation: Kazakhstan. Manufacturer: Surrey. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Leostar-2. USAF Sat Cat: 39731 . COSPAR: 2014-024A. Apogee: 753 km (467 mi). Perigee: 751 km (466 mi). Inclination: 98.52 deg. Period: 99.86 min. Kazakh high resolution imaging satellite; built by Airbus Defense and Space Toulouse, based on the Astrosat bus and had an imager with 1 metre resolution. The third launch of Europe's Vega light launch vehicle..

2014 July 2 - . 09:56 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Thor. Launch Vehicle: Delta 7320-10C.

OCO 2 - . Mass: 407 kg (897 lb). Nation: USA. Spacecraft: Leostar-2. USAF Sat Cat: 40059 . COSPAR: 2014-035A. Apogee: 704 km (437 mi). Perigee: 701 km (435 mi). Inclination: 98.20 deg. Period: 98.83 min. Was to have provided space-based observation of atmospheric carbon dioxide..

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