TDRS-8 (original) (raw)

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American communications satellite

TDRS-8

TDRS-H undergoing processing before launch
Mission type Communication
Operator NASA
COSPAR ID 2000-034A Edit this at Wikidata
SATCAT no. 26388
Mission duration Planned: 11 yearsElapsed: 24 years, 9 months, 24 days
Spacecraft properties
Bus BSS-601
Manufacturer Boeing
Launch mass 3197 kg
Dimensions 21.0 metres long13.1 metres wide
Power 2300 watts
Start of mission
Launch date 30 June 2000, 12:56:00 (2000-06-30UTC12:56) UTC
Rocket Atlas IIA
Launch site Cape Canaveral, LC-36A
Contractor ILS
Orbital parameters
Reference system Geocentric orbit
Regime Geostationary orbit
Longitude 171.0° West (2000-?)270.8° West
Epoch 1 July 2000

TDRS-8, known before launch as TDRS-H, is an American communications satellite, of second generation, which is operated by NASA as part of the Tracking and Data Relay Satellite System. It was constructed by Boeing and is based on the BSS-601 satellite bus.

The launch of TDRS-H

Its launch was contracted by International Launch Services, using an Atlas IIA launch vehicle. The launch occurred on 30 June 2000, at 12:56:00 UTC from Launch Complex 36A at the Cape Canaveral Air Force Station.

It was the first Tracking and Data Relay Satellite, of second generation, to be launched. Due to a malfunction of the multiple-access phased array antenna the spacecraft did not provide the expected level of performance for eighteen of the communications services that it was to provide. The same problem was found and corrected on the TDRS-9 and TDRS-10 satellites prior to their launches.

Following its launch, it raised itself into geostationary orbit by means of its onboard R-4D apogee motor, and was positioned at 150.0° West for on-orbit testing. After testing was complete, it was moved to 171.0° East from where it provides communications services to spacecraft in Earth orbit, including the Space Shuttle and International Space Station.

Location of TDRS as of 26 May 2020

Location of TDRS as of 18 March 2019