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: 17 hours ago
TLE from 17 hours ago
0 TJS-3 AKM
1 43917U 18110C 26017.87277677 .00000029 00000-0 00000-0 0 9993
2 43917 4.2847 80.5255 0005574 129.4384 301.7649 0.98353483 25569Epoch: 2026-01-17T20:56Z
TLE epoch observation values (Epoch: 2026-01-17T20:56:47.912Z)
Latitude
4.08451°
Longitude
80.15042°
Altitude
36,319.714 km
Speed
3.056 km/s
True Right ascension
10h 06m 33s
True Declination
4° 04' 50"
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
14:36:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,357.943 km
Perigee altitude
36,310.327 km
Semi-major axis
42,712.272 km
Eccentricity
0.00056
Inclination
4.2847°
RAAN
80.5255°
Arg. of periapsis
129.4384°
True anomaly
301.71057°
Mean anomaly
301.7649°
Eccentric anomaly
301.73774°
Mean motion
0.24587 °/min
Orbital period
1,464.16 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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