OBJECT A, 44486
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, 44486 is a satellite owned by Qiandao Tansuo (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.
44486 intel report (Beta)
OBJECT A details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 6 hours ago |
| Origin | |
| Manufacturer | Qiandao Tansuo |
| Mission | Commercial Imaging |
| Bus & Motor | QS1, Unknown motor |
| Mass | 65 kg wet, 65 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.5 m |
| Radar Cross Section | 0.375 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 6 hours ago
0 OBJECT A
1 44486U 19052A 24361.18068941 .00059872 00000-0 13640-2 0 9993
2 44486 97.3858 69.6731 0009150 334.6503 25.4294 15.42691056296113Definitive object data (Epoch: 2024-12-26T04:20:11.565Z)
| Latitude | -0.00003° |
| Longitude | -90.53886° |
| Altitude | 435.66 km |
| Speed | 7.654 km/s |
| True Right ascension | 04h 38m 41s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -80.90946° |
| Longitude | -36.61832° |
| Altitude | 463.015 km |
| Speed | 7.636 km/s |
| Apparent Right ascension | 21h 54m 30s |
| Apparent Declination | -70° 10' 36" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:33:00 |
| Azimuth | 183.599° SSW |
| Elevation | -59.61° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 441.34 km |
| Perigee altitude | 428.872 km |
| Semi-major axis | 6,813.243 km |
| Eccentricity | 0.000915 |
| Inclination | 97.3858° |
| RAAN | 69.6731° |
| Arg. of periapsis | 334.6503° |
| True anomaly | 25.47447° |
| Mean anomaly | 25.4294° |
| Eccentric anomaly | 25.45193° |
| Mean motion | 3.85933 °/min |
| BSTAR | 0.001364 |
| Orbital period | 93.28 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 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 | 2024-12-26 17:20:51.798Z | 26.676° NE | 2024-12-26 17:23:51.798Z | 102.51° ESE | 34.848° | 2024-12-26 17:26:51.798Z | 172.554° S |
| 4 mins | 2024-12-27 05:22:51.798Z | 210.86° SW | 2024-12-27 05:24:51.798Z | 266.852° W | 26.354° | 2024-12-27 05:26:51.798Z | 317.333° NNW |
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