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: 7 hours ago
TLE from 7 hours ago
0 OBJECT A
1 62729U 25013A 26036.95845464 .00048563 00000-0 18162-2 0 9995
2 62729 97.6332 211.7066 0010504 33.9956 326.1953 15.27117346 57879Epoch: 2026-02-05T23:00Z
TLE epoch observation values (Epoch: 2026-02-05T23:00:10.480Z)
Latitude
-0.00009°
Longitude
90.55973°
Altitude
481.539 km
Speed
7.628 km/s
True Right ascension
14h 06m 49s
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
07:38:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.606 km
Perigee altitude
474.196 km
Semi-major axis
6,859.538 km
Eccentricity
0.00105
Inclination
97.6332°
RAAN
211.7066°
Arg. of periapsis
33.9956°
True anomaly
326.12826°
Mean anomaly
326.1953°
Eccentric anomaly
326.16179°
Mean motion
3.82033 °/min
Orbital period
94.23 mins
BSTAR
0.0018162
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-06 11:42:38.468Z | 176.16° S | 2026-02-06 11:45:38.468Z | 285.133° WNW | 42.516° | 2026-02-06 11:48:38.468Z | 342.042° N |
| 4 mins | 2026-02-07 00:44:38.468Z | 345.613° N | 2026-02-07 00:45:38.468Z | 315.053° NNW | 35.9° | 2026-02-07 00:48:38.468Z | 214.361° SW |
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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