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 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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63299 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
13 hours ago
Origin
Manufacturer
CAST
Mission
Defense Technology
Bus & Motor
Unknown
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 13 hours ago
0 TJS-15 AKM
1 63299U 25045C 25196.63994557 -.00000071 00000-0 00000+0 0 9994
2 63299 0.3394 91.7771 0019348 55.7409 212.5976 0.98875487 1286Epoch: 2025-07-15T15:21Z
TLE epoch observation values (Epoch: 2025-07-15T15:21:31.297Z)
Latitude
-0.35526°
Longitude
-164.11198°
Altitude
36,251.54 km
Speed
3.055 km/s
True Right ascension
23h 59m 59s
True Declination
0° 21' 18"
Sunlit
Visualization orbit readout
Latitude
0.35371°
Longitude
21.99772°
Altitude
36,117.667 km
Speed
3.065 km/s
Apparent Right ascension
11h 59m 59s
Apparent Declination
-5° 23' 20"
Sunlit
Visualization observer readout
Local Sidereal Time
16:29:52
Azimuth
250.992° W
Elevation
13.433°
Doppler factor
1
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Other satellites on launch #45 in the year 2025 (2025-03-09 UTC)
TJS-15 AKM Visibility forecast
Observer location: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 1042 mins | 2025-07-16 03:53:21.778Z | 250.977° W | 2025-07-16 03:53:21.778Z | 250.977° W | 13.071° | 2025-07-16 21:15:21.778Z | 253.565° W |
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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
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