OBJECT B, 62730
Orbit data source: Space-Track
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 satellite owned by Yunyao yuhang (CN) 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.
62730 intel report (Beta)
OBJECT B details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 11 hours ago |
| Origin | |
| Manufacturer | Yunyao yuhang |
| Mission | Operational spacecraft |
| Bus & Motor | YY-1, Unknown motor |
| Mass | ~50 kg wet, ~50 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 11 hours ago
0 OBJECT B
1 62730U 25013B 25035.71840223 .00009538 00000-0 63142-3 0 9995
2 62730 97.6114 202.6847 0013101 258.1293 101.8466 15.07474144 2312Definitive object data (Epoch: 2025-02-04T17:14:29.952Z)
| Latitude | -0.00001° |
| Longitude | 168.94023° |
| Altitude | 548.862 km |
| Speed | 7.586 km/s |
| True Right ascension | 13h 30m 44s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -82.34751° |
| Longitude | -92.1607° |
| Altitude | 563.399 km |
| Speed | 7.583 km/s |
| Apparent Right ascension | 18h 20m 30s |
| Apparent Declination | -62° 24' 33" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 06:01:09 |
| Azimuth | 185.813° SSW |
| Elevation | -67.318° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 549.977 km |
| Perigee altitude | 531.848 km |
| Semi-major axis | 6,919.05 km |
| Eccentricity | 0.0013101 |
| Inclination | 97.6114° |
| RAAN | 202.6847° |
| Arg. of periapsis | 258.1293° |
| True anomaly | 101.99348° |
| Mean anomaly | 101.8466° |
| Eccentric anomaly | 101.92004° |
| Mean motion | 3.77115 °/min |
| BSTAR | 0.00063142 |
| Orbital period | 95.46 mins |
Other satellites on launch #13 in the year 2025 (2025-01-20 UTC)
| OBJECT A, 62729 |
| OBJECT B, 62730 |
| OBJECT C, 62731 |
| OBJECT D, 62732 |
| OBJECT E, 62733 |
OBJECT B Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-02-05 10:53:23.262Z | 158.341° S | 2025-02-05 10:56:23.262Z | 113.854° SE | 42.416° | 2025-02-05 11:00:23.262Z | 352.88° N |
| 6 mins | 2025-02-06 00:05:23.262Z | 0.031° NNE | 2025-02-06 00:07:23.262Z | 302.788° NW | 41.871° | 2025-02-06 00:11:23.262Z | 203.22° SW |
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