OBJECT B, 44487
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, 44487 is a satellite owned by Guodian Gaokeji (CN) in SSO that was launched on Sat, 17 Aug 2019 UTC via a JIELONG-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.
44487 intel report (Beta)
OBJECT B details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 6 hours ago |
| Origin | |
| Manufacturer | GUOG? |
| Mission | Commercial Communications |
| Bus & Motor | CUBESAT 6U?, Unknown motor |
| Mass | 8 kg wet, 8 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.105 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 6 hours ago
0 OBJECT B
1 44487U 19052B 24361.17259341 .00167108 00000-0 16986-2 0 9997
2 44487 97.3902 76.4989 0007573 304.0874 55.9666 15.64605626296555Definitive object data (Epoch: 2024-12-26T04:08:32.07Z)
| Latitude | -0.00004° |
| Longitude | -80.79052° |
| Altitude | 374.664 km |
| Speed | 7.686 km/s |
| True Right ascension | 05h 05m 59s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -15.59775° |
| Longitude | -78.46195° |
| Altitude | 376.743 km |
| Speed | 7.685 km/s |
| Apparent Right ascension | 02h 14m 55s |
| Apparent Declination | -43° 13' 28" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 09:34:03 |
| Azimuth | 241.842° WSW |
| Elevation | -38.95° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 376.39 km |
| Perigee altitude | 366.168 km |
| Semi-major axis | 6,749.416 km |
| Eccentricity | 0.0007573 |
| Inclination | 97.3902° |
| RAAN | 76.4989° |
| Arg. of periapsis | 304.0874° |
| True anomaly | 56.03855° |
| Mean anomaly | 55.9666° |
| Eccentric anomaly | 56.00257° |
| Mean motion | 3.91421 °/min |
| BSTAR | 0.0016986 |
| Orbital period | 91.97 mins |
Other satellites on launch #52 in the year 2019 (2019-08-17 UTC)
| OBJECT A, 44486 |
| OBJECT B, 44487 |
| OBJECT C, 44488 (Decayed) |
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-26 18:30:54.987Z | 346.945° N | 2024-12-26 18:32:54.987Z | 280.54° WNW | 30.754° | 2024-12-26 18:34:54.987Z | 222.543° SW |
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