OBJECT A, 61869
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, 61869 is a satellite owned by Hangtian Hongtu (CN) in SSO that was launched on Sat, 09 Nov 2024 UTC via a CHANG ZHENG 2C 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.
61869 intel report (Beta)
OBJECT A details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 18 hours ago |
| Origin | |
| Manufacturer | Yinhe |
| Mission | Operational spacecraft |
| Bus & Motor | PIESAT, Unknown motor |
| Mass | 320 kg wet, 320 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 18 hours ago
0 OBJECT A
1 61869U 24203A 24348.16918810 .00011282 00000-0 61276-3 0 9995
2 61869 97.4902 52.4107 0017727 98.8358 261.4882 15.14546928 5143Definitive object data (Epoch: 2024-12-13T04:03:37.851Z)
| Latitude | -0.00005° |
| Longitude | -90.83603° |
| Altitude | 527.267 km |
| Speed | 7.598 km/s |
| True Right ascension | 03h 29m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 82.34896° |
| Longitude | 166.63922° |
| Altitude | 523.647 km |
| Speed | 7.615 km/s |
| Apparent Right ascension | 08h 23m 01s |
| Apparent Declination | 34° 37' 47" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:26:07 |
| Azimuth | 0.663° NNE |
| Elevation | -15.451° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 531.558 km |
| Perigee altitude | 507.104 km |
| Semi-major axis | 6,897.468 km |
| Eccentricity | 0.0017727 |
| Inclination | 97.4902° |
| RAAN | 52.4107° |
| Arg. of periapsis | 98.8358° |
| True anomaly | 261.28737° |
| Mean anomaly | 261.4882° |
| Eccentric anomaly | 261.38778° |
| Mean motion | 3.78886 °/min |
| BSTAR | 0.00061276 |
| Orbital period | 95.02 mins |
Other satellites on launch #203 in the year 2024 (2024-11-09 UTC)
| OBJECT A, 61869 |
| OBJECT B, 61870 |
| OBJECT C, 61871 |
| OBJECT D, 61872 |
| CZ-2C R/B, 61873 |
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-14 03:59:18.826Z | 127.951° SE | 2024-12-14 04:01:18.826Z | 87.162° E | 27.17° | 2024-12-14 04:04:18.826Z | 14.894° NNE |
| 6 mins | 2024-12-14 17:06:18.826Z | 28.704° NE | 2024-12-14 17:08:18.826Z | 73.132° E | 36.922° | 2024-12-14 17:12:18.826Z | 177.193° S |
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