COBE
Satellite information COBE
| Spacetrack Directory Name | COBE |
| Follow COBE | COBE Tracker |
| Pass predictions COBE | Pass predictions COBE |
| Orbit launches |
1989-11-18 (36 years ago)
|
| Days in orbit | 13432 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 871 km |
| Apogee | 883 km |
| Orbit slope (inclination) | 98.9° |
| Laps per day | 14 |
| Height COBE | 886.79 km |
Additional information COBE
COBE, 20322 is a payload satellite owned by GSFC (US) in SSO that was launched on Sat, 18 Nov 1989 UTC via a DELTA 5920-8 launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite COBE Date of exalting 18.11.1989y. Average height of ISS COBE hundred 886.79 km. Average velocity COBE is 26677.29 km/h. Inclination COBE satellite 98.9°.TLE
Average velocity COBE
Average inclination COBE
Mean right ascension of the ascending node (RAAN) COBE
Mean argument of perigee COBE
Mean semi-major axis of the orbit COBE
Mean orbital eccentricity COBE
Frequency COBE
In the table below we show the frequencies COBE.
| Downlink | Mode |
|---|---|
| 2287.500 MHz | FM |
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