| Mission type | Communications |
|---|---|
| Operator | SES |
| COSPAR ID | 2002-053A |
| SATCATno. | 27557 |
| Website | https://www.ses.com/ |
| Mission duration | 15 years (planned) Failed on orbit (DM03 failure) |
| Spacecraft properties | |
| Spacecraft type | Spacebus |
| Bus | Spacebus-3000B3S |
| Manufacturer | Alcatel Space |
| Launch mass | 5,250 kg (11,570 lb) |
| Power | 13kW |
| Start of mission | |
| Launch date | 25 November 2002, 23:04:23UTC |
| Rocket | Proton-K /DM03 |
| Launch site | Baikonur,Site 81/23 |
| Contractor | Khrunichev State Research and Production Space Center |
| Entered service | Failed on orbit (DM03 failure) |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 10 December 2002 |
| Orbital parameters | |
| Reference system | Geocentric orbit[1] |
| Regime | Low Earth orbit Geostationary orbit (planned) |
| Longitude | 19.2° East (planned) |
| Perigee altitude | 142 km (88 mi) |
| Apogee altitude | 288 km (179 mi) |
| Inclination | 51.5° |
| Period | 88.79 minutes |
| Transponders | |
| Band | 54transponders: 52Ku-band 2Ka-band |
| Coverage area | Europe |
Astra 1K was acommunications satellite manufactured byAlcatel Space forSES. When it was launched on 25 November 2002, it was the largest civilian communications satellite ever launched, with a mass of 5,250 kg (11,570 lb).[2] Intended to replace theAstra 1B satellite and provide backup for1A,1C and1D at theAstra 19.2°E orbital position,[3] theBlok DM3 upper stage of theProton-Klaunch vehicle failed to function properly, leaving the satellite in an unusable parking orbit.
Astra 1K was to be a European (Luxembourg-based) geostationary communications satellite that was launched by aProton-K launch vehicle fromBaikonur Cosmodrome at 23:04:23UTC on 25 November 2002. However, theBlok DM3 upper stage attached to the 5,250 kg (11,570 lb), 13kW satellite (reported to be the most massive of civilian communications satellite, with its 52Ku-band and twoKa-band transponders to cover 1,100 channels) was miscommanded to separate after the first burn, resulting in the satellite orbiting at a very low orbit. In an effort to prevent imminent re-entry, the satellite was raised to a circular orbit at an altitude of 288 km, providing sufficient time to select the best course of action. Three options were then under consideration: a) to force its re-entry over thePacific Ocean, b) to retrieve it by aSpace Shuttle, and c) to use up all the fuel on board the satellite to move it to a geostationary orbit at 19.2° east.[4] Although it was suggested that a separately-launched Orbital Recovery Corporation 'space tug' (then in development) might be used to take the satellite to geostationary orbit,[5] the decision was taken in December 2002 to deorbit the satellite, resulting in a huge insurance loss and bringing into question both continued use of the Blok D series of upper stages and the "bigger is better" communications satellite philosophy.[6][2] Astra 1K was intentionally de-orbited on 10 December 2002.[7]
The satellite featured frequency re-use for some of its transponders, using dual patterns coverage, one coveringeastern Europe, the other covering Spain. This design was meant to cover specific markets only, in order to expand the capacity of the fleet, as frequency re-use enables more channels to be transmitted simultaneously at the same frequency, with the drawback that channels broadcast on the Spain beam wouldn't be receivable by any means (no matter how large the receiving dish would be) in the east beam and vice versa. This would have left for example the Netherlands and parts of neighbouring countries without reception of either of the beams, as the beams overlap over those countries, efficiently jamming each other.
Astra 1K also featured multiple Ka-Band capabilities, originally intended to provide an upload path forsatellite Internet access services. SES later developed such a 2-way commercial satellite internet service withASTRA2Connect (now SES Broadband), using Ku-band for upload and download paths.[8]
A replacement satellite,Astra 1KR was successfully launched in 2006.[9]
This article incorporates text from this source, which is in thepublic domain.