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 LEO 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 | LEO |
| 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 24339.18885269 .00139511 00000-0 18229-2 0 9996
2 44487 97.3926 53.5776 0006754 33.4553 326.7128 15.58154773293125Definitive object data (Epoch: 2024-12-04T04:31:56.872Z)
| Latitude | -0.00005° |
| Longitude | -87.89694° |
| Altitude | 392.317 km |
| Speed | 7.677 km/s |
| True Right ascension | 03h 34m 18s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -77.32339° |
| Longitude | 57.34822° |
| Altitude | 423.618 km |
| Speed | 7.654 km/s |
| Apparent Right ascension | 18h 59m 26s |
| Apparent Declination | -65° 56' 52" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:10:26 |
| Azimuth | 164.606° S |
| Elevation | -62.088° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 394.483 km |
| Perigee altitude | 385.341 km |
| Semi-major axis | 6,768.049 km |
| Eccentricity | 0.0006754 |
| Inclination | 97.3926° |
| RAAN | 53.5776° |
| Arg. of periapsis | 33.4553° |
| True anomaly | 326.67029° |
| Mean anomaly | 326.7128° |
| Eccentric anomaly | 326.69155° |
| Mean motion | 3.89805 °/min |
| BSTAR | 0.0018229 |
| Orbital period | 92.35 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 | 2024-12-04 17:26:01.329Z | 51.059° ENE | 2024-12-04 17:28:01.329Z | 101.387° ESE | 20.308° | 2024-12-04 17:30:01.329Z | 146.451° SSE |
| 4 mins | 2024-12-05 05:20:01.329Z | 177.117° S | 2024-12-05 05:22:01.329Z | 307.614° NW | 41.933° | 2024-12-05 05:24:01.329Z | 342.33° N |
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