CAMEO & DELTA 1 R/B
Satellite information CAMEO & DELTA 1 R/B
| Spacetrack Directory Name | CAMEO & DELTA 1 R/B |
| Follow CAMEO & DELTA 1 R/B | CAMEO & DELTA 1 R/B Tracker |
| Pass predictions CAMEO & DELTA 1 R/B | Pass predictions CAMEO & DELTA 1 R/B |
| Orbit launches |
1978-10-24 (47 years ago)
|
| Days in orbit | 17476 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 922 km |
| Apogee | 966 km |
| Orbit slope (inclination) | 99.42° |
| Laps per day | 14 |
| Height CAMEO & DELTA 1 R/B | 954.14 km |
Additional information CAMEO & DELTA 1 R/B
DELTA 1 R/B(+CAMEO), 11081 is space debris in SSO originally from a launch on Tue, 24 Oct 1978 UTC via a DELTA 2910 launch vehicle from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite CAMEO & DELTA 1 R/B Date of exalting 24.10.1978y. Average height of ISS CAMEO & DELTA 1 R/B hundred 954.14 km. Average velocity CAMEO & DELTA 1 R/B is 26554.38 km/h. Inclination CAMEO & DELTA 1 R/B satellite 99.42°.TLE
Average velocity CAMEO & DELTA 1 R/B
Average inclination CAMEO & DELTA 1 R/B
Mean right ascension of the ascending node (RAAN) CAMEO & DELTA 1 R/B
Mean argument of perigee CAMEO & DELTA 1 R/B
Mean semi-major axis of the orbit CAMEO & DELTA 1 R/B
Mean orbital eccentricity CAMEO & DELTA 1 R/B
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