CHOLLIMA-1 R/B
Satellite information CHOLLIMA-1 R/B
| Spacetrack Directory Name | CHOLLIMA-1 R/B |
| Follow CHOLLIMA-1 R/B | CHOLLIMA-1 R/B Tracker |
| Pass predictions CHOLLIMA-1 R/B | Pass predictions CHOLLIMA-1 R/B |
| Orbit launches |
2023-11-21 (2 years ago)
|
| Days in orbit | 1034 |
| Country/organisation of origin | Korea (NKOR) |
| Starting point | YUN (Sohae Satellite Launching Station, North Korea) |
| Perigee | 417 km |
| Apogee | 445 km |
| Orbit slope (inclination) | 97.3° |
| Laps per day | 16 |
| Height CHOLLIMA-1 R/B | 375.59 km |
Additional information CHOLLIMA-1 R/B
CHOLLIMA-1 R/B, 58401 is space debris in SSO originally from a launch on Tue, 21 Nov 2023 UTC launched from the Yunsong, Dprk (YUN). 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 CHOLLIMA-1 R/B Date of exalting 21.11.2023y. Average height of ISS CHOLLIMA-1 R/B hundred 375.59 km. Average velocity CHOLLIMA-1 R/B is 27668.68 km/h. Inclination CHOLLIMA-1 R/B satellite 97.3°.TLE
Average velocity CHOLLIMA-1 R/B
Average inclination CHOLLIMA-1 R/B
Mean right ascension of the ascending node (RAAN) CHOLLIMA-1 R/B
Mean argument of perigee CHOLLIMA-1 R/B
Mean semi-major axis of the orbit CHOLLIMA-1 R/B
Mean orbital eccentricity CHOLLIMA-1 R/B
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