OBJECT B, 62730
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 B, 62730 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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62730 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, 0.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT B
1 62730U 25013B 25342.22993837 .00006255 00000-0 39307-3 0 9991
2 62730 97.6376 146.8210 0012769 307.4737 52.5330 15.09543418 48501Epoch: 2025-12-08T05:31Z
TLE epoch observation values (Epoch: 2025-12-08T05:31:06.675Z)
Latitude
0.00001°
Longitude
-13.18877°
Altitude
535.298 km
Speed
7.598 km/s
True Right ascension
09h 47m 17s
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
13:26:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.411 km
Perigee altitude
525.757 km
Semi-major axis
6,912.721 km
Eccentricity
0.00128
Inclination
97.6376°
RAAN
146.821°
Arg. of periapsis
307.4737°
True anomaly
52.64925°
Mean anomaly
52.533°
Eccentric anomaly
52.59111°
Mean motion
3.77633 °/min
Orbital period
95.33 mins
BSTAR
0.00039307
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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 B 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 | 2025-12-08 23:35:26.949Z | 32.076° NE | 2025-12-08 23:38:26.949Z | 101.737° ESE | 33.201° | 2025-12-08 23:41:26.949Z | 166.283° S |
| 4 mins | 2025-12-09 10:19:26.949Z | 94.786° ESE | 2025-12-09 10:20:26.949Z | 74.255° E | 19.254° | 2025-12-09 10:23:26.949Z | 21.425° NNE |
| 4 mins | 2025-12-09 11:53:26.949Z | 226.682° WSW | 2025-12-09 11:55:26.949Z | 275.516° WNW | 23.392° | 2025-12-09 11:57:26.949Z | 313.623° NW |
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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