IRS P2 R/B
Satellite information IRS P2 R/B
| Spacetrack Directory Name | IRS P2 R/B |
| Follow IRS P2 R/B | IRS P2 R/B Tracker |
| Pass predictions IRS P2 R/B | Pass predictions IRS P2 R/B |
| Orbit launches |
1994-10-15 (31 years ago)
|
| Days in orbit | 11658 |
| Country/organisation of origin | Indie (IND) |
| Starting point | SRILR (Satish Dhawan Space Centre, India) |
| Perigee | 794 km |
| Apogee | 876 km |
| Orbit slope (inclination) | 98.84° |
| Laps per day | 14 |
| Height IRS P2 R/B | 846.11 km |
Additional information IRS P2 R/B
IRS P2 R/B, 23324 is space debris in SSO originally from a launch on Sat, 15 Oct 1994 UTC launched from the Sirharikota (SRI). 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 IRS P2 R/B Date of exalting 15.10.1994y. Average height of ISS IRS P2 R/B hundred 846.11 km. Average velocity IRS P2 R/B is 26752.32 km/h. Inclination IRS P2 R/B satellite 98.84°.TLE
Average velocity IRS P2 R/B
Average inclination IRS P2 R/B
Mean right ascension of the ascending node (RAAN) IRS P2 R/B
Mean argument of perigee IRS P2 R/B
Mean semi-major axis of the orbit IRS P2 R/B
Mean orbital eccentricity IRS P2 R/B
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