TAIJING-2 04

58820
Spacetrack Directory Number
2024-01-23
Orbit launches
426.89 km
Average height
27564.26 km/h
Average velocity


Satellite information TAIJING-2 04 - 2024-016A

Spacetrack Directory Name TAIJING-2 04
Alternative name 2024-016A
Follow TAIJING-2 04 TAIJING-2 04 Tracker
Pass predictions TAIJING-2 04 Pass predictions TAIJING-2 04
Orbit launches 2024-01-23 g.01:00 (2 years ago)
Days in orbit 989
Country/organisation of origin Chiny (PRC)
Starting point JSC (Jiuquan Satellite Launch Center, China)
Perigee 524 km
Apogee 542 km
Orbit slope (inclination) 97.45°
Laps per day 16
Height TAIJING-2 04 426.89 km

Additional information TAIJING-2 04

OBJECT A, 58820 is a satellite owned by Weina (CN) in SSO that was launched on Tue, 23 Jan 2024 UTC via a LIJIAN-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earths orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earths gravity.

satellite TAIJING-2 04 Date of exalting 23.01.2024y. Average height of ISS TAIJING-2 04 hundred 426.89 km. Average velocity TAIJING-2 04 is 27564.26 km/h. Inclination TAIJING-2 04 satellite 97.45°.

TLE

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Average orbit height TAIJING-2 04

Average velocity TAIJING-2 04

Average inclination TAIJING-2 04

Mean right ascension of the ascending node (RAAN) TAIJING-2 04

Mean argument of perigee TAIJING-2 04

Mean semi-major axis of the orbit TAIJING-2 04

Mean orbital eccentricity TAIJING-2 04

Frequency TAIJING-2 04

In the table below we show the frequencies TAIJING-2 04.

Downlink Mode
401.950 MHz FM

Update time: 2026-10-07 21:10:23
Average height of ISS TAIJING-2 04 is: 426.89km
Average velocity TAIJING-2 04 is: 27564.26km/h
Average orbit height TAIJING-2 04 is: 97.45°
TAIJING-2 04 a new group of Starlink satellites has been launched 2024-01-23
TAIJING-2 04 is from 989 days Days in orbit.