OBJECT A, 61617
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
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, 61617 is a satellite owned by PLA GAD (CN) in LEO that was launched on Wed, 23 Oct 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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61617 intel report (Beta)
OBJECT A details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 21 hours ago |
| Origin | |
| Manufacturer | SAST |
| Mission | Spacecraft |
| Bus & Motor | Unknown |
| Mass | ~300 kg wet, ~300 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 21 hours ago
0 OBJECT A
1 61617U 24190A 25001.82162852 .00031895 00000-0 13095-2 0 9995
2 61617 34.9927 299.8098 0007201 228.4892 131.5205 15.23241489 10802Epoch: 2025-01-01T19:43Z
Definitive object data (Epoch: 2025-01-01T19:43:08.704Z)
| Latitude | -0.00001° |
| Longitude | -97.68588° |
| Altitude | 498.26 km |
| Speed | 7.616 km/s |
| True Right ascension | 19h 59m 14s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 6.96624° |
| Longitude | 66.76485° |
| Altitude | 492.376 km |
| Speed | 7.623 km/s |
| Apparent Right ascension | 06h 01m 41s |
| Apparent Declination | -16° 05' 27" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 16:43:54 |
| Azimuth | 319.06° NNW |
| Elevation | -60.778° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 504.275 km |
| Perigee altitude | 494.37 km |
| Semi-major axis | 6,877.46 km |
| Eccentricity | 0.0007201 |
| Inclination | 34.9927° |
| RAAN | 299.8098° |
| Arg. of periapsis | 228.4892° |
| True anomaly | 131.58225° |
| Mean anomaly | 131.5205° |
| Eccentric anomaly | 131.55138° |
| Mean motion | 3.80541 °/min |
| BSTAR | 0.0013095 |
| Orbital period | 94.6 mins |
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Other satellites on launch #190 in the year 2024 (2024-10-23 UTC)
| OBJECT A, 61617 |
| OBJECT B, 61618 |
| OBJECT C, 61619 |
| CZ-2C R/B, 61620 (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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-01-03 00:20:03.816Z | 212.195° SW | 2025-01-03 00:22:03.816Z | 157.156° SSE | 27.122° | 2025-01-03 00:25:03.816Z | 105.898° ESE |
| 5 mins | 2025-01-03 01:59:03.816Z | 240.423° WSW | 2025-01-03 02:01:03.816Z | 188.333° SSW | 31.644° | 2025-01-03 02:04:03.816Z | 119.517° SE |
| 4 mins | 2025-01-03 03:39:03.816Z | 230.585° WSW | 2025-01-03 03:40:03.816Z | 210.129° SW | 20.168° | 2025-01-03 03:43:03.816Z | 152° SSE |
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