OBJECT B, 61615
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 B, 61615 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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61615 intel report (Beta)
OBJECT B details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 12 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 12 hours ago
0 OBJECT B
1 61615U 24189B 25002.45157839 .00010620 00000-0 83889-3 0 9992
2 61615 97.6066 31.9905 0006759 61.6714 298.5191 15.00841006 10836Epoch: 2025-01-02T10:50Z
Definitive object data (Epoch: 2025-01-02T10:50:16.372Z)
| Latitude | -0.00007° |
| Longitude | 127.09198° |
| Altitude | 565.122 km |
| Speed | 7.58 km/s |
| True Right ascension | 02h 07m 57s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 3.91961° |
| Longitude | -51.89803° |
| Altitude | 568.956 km |
| Speed | 7.576 km/s |
| Apparent Right ascension | 12h 45m 34s |
| Apparent Declination | -18° 42' 42" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 22:39:59 |
| Azimuth | 298.927° NW |
| Elevation | -55.682° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 565.992 km |
| Perigee altitude | 556.611 km |
| Semi-major axis | 6,939.439 km |
| Eccentricity | 0.0006759 |
| Inclination | 97.6066° |
| RAAN | 31.9905° |
| Arg. of periapsis | 61.6714° |
| True anomaly | 298.45102° |
| Mean anomaly | 298.5191° |
| Eccentric anomaly | 298.48506° |
| Mean motion | 3.75454 °/min |
| BSTAR | 0.00083889 |
| Orbital period | 95.88 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 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-01-03 01:22:10.028Z | 139.461° SSE | 2025-01-03 01:25:10.028Z | 82.705° E | 32.378° | 2025-01-03 01:28:10.028Z | 9.559° NNE |
| 6 mins | 2025-01-03 14:37:10.028Z | 17.504° NNE | 2025-01-03 14:39:10.028Z | 42.694° NE | 42.813° | 2025-01-03 14:43:10.028Z | 188.508° SSW |
Authenticating...
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