OBJECT A, 62729
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 A, 62729 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.
62729 intel report (Beta)
OBJECT A details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 9 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 9 hours ago
0 OBJECT A
1 62729U 25013A 25035.77901563 .00025324 00000-0 15539-2 0 9991
2 62729 97.6106 202.7570 0013568 232.2072 127.7929 15.10027008 2318Definitive object data (Epoch: 2025-02-04T18:41:46.95Z)
| Latitude | -0.00004° |
| Longitude | 147.13197° |
| Altitude | 544.947 km |
| Speed | 7.587 km/s |
| True Right ascension | 13h 31m 01s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -75.47913° |
| Longitude | -63.35971° |
| Altitude | 555.028 km |
| Speed | 7.588 km/s |
| Apparent Right ascension | 19h 04m 47s |
| Apparent Declination | -63° 36' 32" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:48:51 |
| Azimuth | 199.109° SSW |
| Elevation | -63.789° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 542.483 km |
| Perigee altitude | 523.728 km |
| Semi-major axis | 6,911.243 km |
| Eccentricity | 0.0013568 |
| Inclination | 97.6106° |
| RAAN | 202.757° |
| Arg. of periapsis | 232.2072° |
| True anomaly | 127.91564° |
| Mean anomaly | 127.7929° |
| Eccentric anomaly | 127.85428° |
| Mean motion | 3.77754 °/min |
| BSTAR | 0.0015539 |
| Orbital period | 95.3 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 A 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-02-05 10:44:07.166Z | 146.175° SSE | 2025-02-05 10:47:07.166Z | 61.495° ENE | 38° | 2025-02-05 10:50:07.166Z | 0.347° NNE |
| 6 mins | 2025-02-05 23:54:07.166Z | 12.408° NNE | 2025-02-05 23:56:07.166Z | 12.892° NNE | 44.112° | 2025-02-06 00:00:07.166Z | 193.297° SSW |
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