OBJECT A, 62729
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
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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Edit Public Description
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, 0.4 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 OBJECT A
1 62729U 25013A 25341.26581732 .00036878 00000-0 15490-2 0 9999
2 62729 97.6312 149.8304 0010178 252.0757 107.9370 15.23300455 48625Epoch: 2025-12-07T06:22Z
TLE epoch observation values (Epoch: 2025-12-07T06:22:46.616Z)
Latitude
-0.00001°
Longitude
-22.14551°
Altitude
501.143 km
Speed
7.613 km/s
True Right ascension
09h 59m 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
23:02:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.858 km
Perigee altitude
485.871 km
Semi-major axis
6,871.002 km
Eccentricity
0.00102
Inclination
97.6312°
RAAN
149.8304°
Arg. of periapsis
252.0757°
True anomaly
108.04792°
Mean anomaly
107.937°
Eccentric anomaly
107.99246°
Mean motion
3.81077 °/min
Orbital period
94.47 mins
BSTAR
0.001549
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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 | 2025-12-08 10:53:51.398Z | 129.87° SE | 2025-12-08 10:56:51.398Z | 56.074° ENE | 27.314° | 2025-12-08 10:58:51.398Z | 15.032° NNE |
| 5 mins | 2025-12-08 23:56:51.398Z | 35.474° NE | 2025-12-08 23:58:51.398Z | 92.176° ESE | 34.853° | 2025-12-09 00:01:51.398Z | 169.587° 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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