OBJECT C, 61616
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 C, 61616 is a satellite owned by ZJUNI-SAT (CN) in SSO that was launched on Tue, 22 Oct 2024 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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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61616 intel report (Beta)
OBJECT C details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 14 hours ago |
| Origin | |
| Manufacturer | ZJUNI-SAT |
| Mission | Spacecraft |
| Bus & Motor | TP-3, Unknown motor |
| Mass | 200 kg wet, ~200 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 14 hours ago
0 OBJECT C
1 61616U 24189C 25002.37509724 .00011022 00000-0 86194-3 0 9997
2 61616 97.6081 31.9337 0005565 65.3716 294.8088 15.01223416 10823Epoch: 2025-01-02T09:00Z
Definitive object data (Epoch: 2025-01-02T09:00:08.401Z)
| Latitude | 0.00002° |
| Longitude | 154.64376° |
| Altitude | 564.562 km |
| Speed | 7.58 km/s |
| True Right ascension | 02h 07m 44s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -40.23753° |
| Longitude | -31.24835° |
| Altitude | 582.085 km |
| Speed | 7.566 km/s |
| Apparent Right ascension | 12h 14m 54s |
| Apparent Declination | -42° 19' 09" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 22:37:30 |
| Azimuth | 254.572° W |
| Elevation | -71.562° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 563.983 km |
| Perigee altitude | 556.261 km |
| Semi-major axis | 6,938.259 km |
| Eccentricity | 0.0005565 |
| Inclination | 97.6081° |
| RAAN | 31.9337° |
| Arg. of periapsis | 65.3716° |
| True anomaly | 294.7509° |
| Mean anomaly | 294.8088° |
| Eccentric anomaly | 294.77985° |
| Mean motion | 3.7555 °/min |
| BSTAR | 0.00086194 |
| Orbital period | 95.86 mins |
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Other satellites on launch #189 in the year 2024 (2024-10-22 UTC)
| OBJECT A, 61614 |
| OBJECT B, 61615 |
| OBJECT C, 61616 |
OBJECT C 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 01:08:41.799Z | 121.509° SE | 2025-01-03 01:11:41.799Z | 58.742° ENE | 24.288° | 2025-01-03 01:13:41.799Z | 20.901° NNE |
| 4 mins | 2025-01-03 02:44:41.799Z | 234.983° WSW | 2025-01-03 02:46:41.799Z | 275.296° WNW | 19.012° | 2025-01-03 02:48:41.799Z | 308.884° NW |
| 6 mins | 2025-01-03 14:22:41.799Z | 30.874° NE | 2025-01-03 14:24:41.799Z | 74.302° E | 36.435° | 2025-01-03 14:28:41.799Z | 174.925° S |
Authenticating...
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