TJS-15 AKM, 63299
Orbit data source: Space-Track
TJS-15 AKM, 63299 is space debris in GEO originally from a launch on Sun, 09 Mar 2025 UTC launched 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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63299 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TJS-15 AKM
1 63299U 25045C 25307.89017868 -.00000175 00000-0 00000+0 0 9992
2 63299 0.6300 88.3850 0018504 68.9825 202.7532 0.98876209 2381Epoch: 2025-11-03T21:21Z
TLE epoch observation values (Epoch: 2025-11-03T21:21:51.437Z)
Latitude
-0.60626°
Longitude
-3.84938°
Altitude
36,254.629 km
Speed
3.055 km/s
True Right ascension
00h 00m 00s
True Declination
0° 36' 20"
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
09:30:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,262.237 km
Perigee altitude
36,104.725 km
Semi-major axis
42,561.618 km
Eccentricity
0.00185
Inclination
0.63°
RAAN
88.385°
Arg. of periapsis
68.9825°
True anomaly
202.67137°
Mean anomaly
202.7532°
Eccentric anomaly
202.71227°
Mean motion
0.24718 °/min
Orbital period
1,456.42 mins
BSTAR
0
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Other satellites on launch #45 in the year 2025 (2025-03-09 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-15 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-15 AKM is likely not visible in the next few days. |
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63299 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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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 ascending order |
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