CELESTIS 02/TAURUS R/B
Satellite information CELESTIS 02/TAURUS R/B
| Spacetrack Directory Name | CELESTIS 02/TAURUS R/B |
| Alternative name | CELESTIS-02 & TAURUS R/B |
| Follow CELESTIS 02/TAURUS R/B | CELESTIS 02/TAURUS R/B Tracker |
| Pass predictions CELESTIS 02/TAURUS R/B | Pass predictions CELESTIS 02/TAURUS R/B |
| Orbit launches |
1998-02-10 (28 years ago)
|
| Days in orbit | 10423 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Categories | |
| Perigee | 775 km |
| Apogee | 865 km |
| Orbit slope (inclination) | 108.01° |
| Laps per day | 14 |
| Height CELESTIS 02/TAURUS R/B | 828.02 km |
Additional information CELESTIS 02/TAURUS R/B
CELESTIS 02/TAURUS R/B, 25160 is space debris in LEO originally from a launch on Tue, 10 Feb 1998 UTC launched 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 CELESTIS 02/TAURUS R/B Date of exalting 10.02.1998y. Average height of ISS CELESTIS 02/TAURUS R/B hundred 828.02 km. Average velocity CELESTIS 02/TAURUS R/B is 26786.31 km/h. Inclination CELESTIS 02/TAURUS R/B satellite 108.01°.TLE
Average orbit height CELESTIS 02/TAURUS R/B
Average velocity CELESTIS 02/TAURUS R/B
Average inclination CELESTIS 02/TAURUS R/B
Mean right ascension of the ascending node (RAAN) CELESTIS 02/TAURUS R/B
Mean argument of perigee CELESTIS 02/TAURUS R/B
Mean semi-major axis of the orbit CELESTIS 02/TAURUS R/B
Mean orbital eccentricity CELESTIS 02/TAURUS R/B
ISS
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