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: 5 hours ago
TLE from 5 hours ago
0 OBJECT A
1 62729U 25013A 25311.82058751 .00029544 00000-0 13077-2 0 9999
2 62729 97.6319 119.9312 0011377 356.9471 3.1693 15.21558045 44144Epoch: 2025-11-07T19:41Z
TLE epoch observation values (Epoch: 2025-11-07T19:41:38.760Z)
Latitude
-0.00004°
Longitude
137.26064°
Altitude
496.41 km
Speed
7.621 km/s
True Right ascension
07h 59m 43s
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
21:05:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.937 km
Perigee altitude
490.291 km
Semi-major axis
6,876.251 km
Eccentricity
0.00114
Inclination
97.6319°
RAAN
119.9312°
Arg. of periapsis
356.9471°
True anomaly
3.17652°
Mean anomaly
3.1693°
Eccentric anomaly
3.17291°
Mean motion
3.80641 °/min
Orbital period
94.58 mins
BSTAR
0.0013077
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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 | 2025-11-08 00:59:01.098Z | 341.936° N | 2025-11-08 01:02:01.098Z | 284.077° WNW | 21.572° | 2025-11-08 01:04:01.098Z | 244.374° WSW |
| 5 mins | 2025-11-08 11:37:01.098Z | 187.073° SSW | 2025-11-08 11:39:01.098Z | 256.281° W | 40.257° | 2025-11-08 11:42:01.098Z | 337.337° NNW |
| 5 mins | 2025-11-09 00:41:01.098Z | 337.827° N | 2025-11-09 00:43:01.098Z | 266.919° W | 31.682° | 2025-11-09 00:46:01.098Z | 216.934° SW |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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