SJ-21 AKM, 49382
Orbit data source: Space-Track
SJ-21 AKM, 49382 is space debris in GEO originally from a launch on Sun, 24 Oct 2021 UTC via a CHANG ZHENG 3B launch vehicle from the Xichang Space Center, China (XSC). 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.
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49382 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SJ-21 AKM
1 49382U 21094C 25337.99840235 -.00000222 00000-0 00000+0 0 9998
2 49382 10.9135 41.3133 0004218 180.8849 196.3758 0.99219693 15558Epoch: 2025-12-03T23:57Z
TLE epoch observation values (Epoch: 2025-12-03T23:57:41.963Z)
Latitude
3.23842°
Longitude
-14.2347°
Altitude
36,100.578 km
Speed
3.063 km/s
True Right ascension
03h 53m 00s
True Declination
3° 14' 07"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:59:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,103.056 km
Perigee altitude
36,067.234 km
Semi-major axis
42,463.282 km
Eccentricity
0.00042
Inclination
10.9135°
RAAN
41.3133°
Arg. of periapsis
180.8849°
True anomaly
196.36218°
Mean anomaly
196.3758°
Eccentric anomaly
196.36899°
Mean motion
0.24804 °/min
Orbital period
1,451.38 mins
BSTAR
0
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Other satellites on launch #94 in the year 2021 (2021-10-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SJ-21 AKM Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| SJ-21 AKM is likely not visible in the next few days. |
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49382 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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