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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Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 TJS-3 AKM
1 43917U 18110C 26108.25797181 -.00000179 00000-0 00000-0 0 9990
2 43917 4.5229 79.2434 0004904 125.6796 270.8535 0.98356561 26450Epoch: 2026-04-18T06:11Z
TLE epoch observation values (Epoch: 2026-04-18T06:11:28.764Z)
Latitude
2.67026°
Longitude
176.37679°
Altitude
36,331.115 km
Speed
3.055 km/s
True Right ascension
07h 42m 30s
True Declination
2° 40' 03"
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
21:14:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,354.189 km
Perigee altitude
36,312.297 km
Semi-major axis
42,711.38 km
Eccentricity
0.00049
Inclination
4.5229°
RAAN
79.2434°
Arg. of periapsis
125.6796°
True anomaly
270.79731°
Mean anomaly
270.8535°
Eccentric anomaly
270.82541°
Mean motion
0.24588 °/min
Orbital period
1,464.11 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
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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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| TJS-3 AKM is likely not visible in the next few days. |
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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 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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