OBJECT A, 62729
Orbit data source: Space-Track
OBJECT A, 62729 is a Chinese satellite in SSO that was launched on Mon, 20 Jan 2025 UTC via a GUSHENXING 1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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62729 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OBJECT A
1 62729U 25013A 26306.59144808 .00026044 00000-0 58498-3 0 9996
2 62729 97.6356 131.0827 0007424 154.1688 205.9931 15.43318677 99244Epoch: 2026-11-02T14:11Z
TLE epoch observation values (Epoch: 2026-11-02T14:11:41.114Z)
Latitude
-0.00001°
Longitude
-123.70487°
Altitude
443.987 km
Speed
7.643 km/s
True Right ascension
08h 44m 19s
True Declination
0° 00' 00"
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
06:17:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
438.324 km
Perigee altitude
428.211 km
Semi-major axis
6,811.405 km
Eccentricity
0.00074
Inclination
97.6356°
RAAN
131.0827°
Arg. of periapsis
154.1688°
True anomaly
205.95585°
Mean anomaly
205.9931°
Eccentric anomaly
205.97447°
Mean motion
3.8609 °/min
Orbital period
93.24 mins
BSTAR
0.00058498
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Other satellites on launch #13 in the year 2025 (2025-01-20 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.OBJECT A 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-03 12:06:52.117Z | 141.037° SSE | 2026-11-03 12:09:52.117Z | 54.339° ENE | 38.46° | 2026-11-03 12:11:52.117Z | 8.32° NNE |
| 4 mins | 2026-11-04 01:00:52.117Z | 49.419° ENE | 2026-11-04 01:01:52.117Z | 87.188° E | 40.504° | 2026-11-04 01:04:52.117Z | 169.545° S |
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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