TJS-3 AKM, 43917
Orbit data source: Space-Track
TJS-3 AKM, 43917 is space debris in GEO originally from a launch on Mon, 24 Dec 2018 UTC via a CHANG ZHENG 3C 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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43917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Non-operational Defense Technology
Bus & Motor
Unknown
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.5 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 TJS-3 AKM
1 43917U 18110C 25261.30669721 -.00000125 00000-0 00000-0 0 9994
2 43917 3.9619 82.1615 0006575 114.3145 110.4207 0.98355959 24362Epoch: 2025-09-18T07:21Z
TLE epoch observation values (Epoch: 2025-09-18T07:21:38.638Z)
Latitude
-2.7769°
Longitude
-160.98573°
Altitude
36,342.228 km
Speed
3.054 km/s
True Right ascension
20h 27m 34s
True Declination
-2° 46' 27"
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
10:42:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,361.502 km
Perigee altitude
36,305.337 km
Semi-major axis
42,711.557 km
Eccentricity
0.00066
Inclination
3.9619°
RAAN
82.1615°
Arg. of periapsis
114.3145°
True anomaly
110.49129°
Mean anomaly
110.4207°
Eccentric anomaly
110.456°
Mean motion
0.24588 °/min
Orbital period
1,464.12 mins
BSTAR
0
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Other satellites on launch #110 in the year 2018 (2018-12-24 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.TJS-3 AKM Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 830 mins | 2025-09-18 17:51:07.336Z | 249.95° W | 2025-09-18 21:45:07.336Z | 252.815° W | 16.234° | 2025-09-19 07:41:07.336Z | 249.716° W |
| 35 mins | 2025-09-19 17:16:07.336Z | 254.102° W | 2025-09-19 17:51:07.336Z | 254.695° W | 10.26° | 2025-09-19 17:51:07.336Z | 254.695° W |
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43917 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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