DELTA 1 R/B(+CAMEO)
Satellite information DELTA 1 R/B(+CAMEO) - CAMEO & DELTA 1 R/B
| Spacetrack Directory Name | DELTA 1 R/B(+CAMEO) |
| Alternative name | CAMEO & DELTA 1 R/B |
| Follow DELTA 1 R/B(+CAMEO) | DELTA 1 R/B(+CAMEO) Tracker |
| Pass predictions DELTA 1 R/B(+CAMEO) | Pass predictions DELTA 1 R/B(+CAMEO) |
| Orbit launches |
1978-10-24 (47 years ago)
|
| Days in orbit | 17516 |
| 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 DELTA 1 R/B(+CAMEO) | 954.09 km |
Additional information DELTA 1 R/B(+CAMEO)
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 DELTA 1 R/B(+CAMEO) Date of exalting 24.10.1978y. Average height of ISS DELTA 1 R/B(+CAMEO) hundred 954.09 km. Average velocity DELTA 1 R/B(+CAMEO) is 26554.56 km/h. Inclination DELTA 1 R/B(+CAMEO) satellite 99.42°.TLE
Average velocity DELTA 1 R/B(+CAMEO)
Average inclination DELTA 1 R/B(+CAMEO)
Mean right ascension of the ascending node (RAAN) DELTA 1 R/B(+CAMEO)
Mean argument of perigee DELTA 1 R/B(+CAMEO)
Mean semi-major axis of the orbit DELTA 1 R/B(+CAMEO)
Mean orbital eccentricity DELTA 1 R/B(+CAMEO)
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