OBJECT A, 60088
Orbit data source: Space-Track
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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, 60088 is a Chinese satellite in LEO that was launched on Sat, 22 Jun 2024 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). 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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60088 intel report (Beta)
OBJECT A details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 18 hours ago |
| Origin | |
| Manufacturer | IMI/CAS |
| Mission | Operational Civil Astronomy |
| Bus & Motor | SVOM, Unknown motor |
| Mass | 930 kg wet, 930 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 2 Pan, 10 m |
| Radar Cross Section | 5.372 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 OBJECT A
1 60088U 24116A 25014.72323435 .00003065 00000-0 36336-3 0 9995
2 60088 28.9941 148.3256 0004248 166.4952 193.5755 14.81947280 30593Epoch: 2025-01-14T17:21Z
Definitive object data (Epoch: 2025-01-14T17:21:27.447Z)
| Latitude | -0.00003° |
| Longitude | 133.53535° |
| Altitude | 624.413 km |
| Speed | 7.547 km/s |
| True Right ascension | 09h 53m 18s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 26.59049° |
| Longitude | -115.2078° |
| Altitude | 620.377 km |
| Speed | 7.554 km/s |
| Apparent Right ascension | 20h 12m 22s |
| Apparent Declination | -7° 55' 14" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:18:59 |
| Azimuth | 77.325° E |
| Elevation | -26.686° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 630.24 km |
| Perigee altitude | 624.288 km |
| Semi-major axis | 7,005.401 km |
| Eccentricity | 0.0004248 |
| Inclination | 28.9941° |
| RAAN | 148.3256° |
| Arg. of periapsis | 166.4952° |
| True anomaly | 193.56408° |
| Mean anomaly | 193.5755° |
| Eccentric anomaly | 193.56979° |
| Mean motion | 3.70164 °/min |
| BSTAR | 0.00036336 |
| Orbital period | 97.25 mins |
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Other satellites on launch #116 in the year 2024 (2024-06-22 UTC)
| OBJECT A, 60088 |
| OBJECT B, 60089 |
| CZ-2C R/B, 60090 (Decayed) |
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-01-15 13:01:45.414Z | 195.876° SSW | 2025-01-15 13:03:45.414Z | 168.254° S | 14.65° | 2025-01-15 13:05:45.414Z | 139.737° SSE |
| 4 mins | 2025-01-15 14:44:45.414Z | 206.03° SW | 2025-01-15 14:46:45.414Z | 171.031° S | 19.098° | 2025-01-15 14:48:45.414Z | 140.877° SSE |
Authenticating...
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