OBJECT P, 61907
Orbit data source: Space-Track
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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT P, 61907 is a Chinese satellite in SSO that was launched on Mon, 11 Nov 2024 UTC via a LIJIAN-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.
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61907 intel report (Beta)
OBJECT P details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 17 hours ago |
| Origin | |
| Manufacturer | JUNT |
| Mission | Operational spacecraft |
| Bus & Motor | CUBESAT 6U?, Unknown motor |
| Mass | ~12 kg wet, ~12 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 17 hours ago
0 OBJECT P
1 61907U 24205P 24348.17811443 .00006570 00000-0 34977-3 0 9997
2 61907 97.4754 59.8292 0014925 173.8066 186.3354 15.15465933 4813Epoch: 2024-12-13T04:16Z
Definitive object data (Epoch: 2024-12-13T04:16:29.086Z)
| Latitude | -0.00002° |
| Longitude | -86.63981° |
| Altitude | 532.881 km |
| Speed | 7.591 km/s |
| True Right ascension | 03h 59m 19s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 14.38692° |
| Longitude | -87.84086° |
| Altitude | 531.343 km |
| Speed | 7.593 km/s |
| Apparent Right ascension | 05h 43m 19s |
| Apparent Declination | -13° 35' 33" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 20:17:58 |
| Azimuth | 63.199° ENE |
| Elevation | -47.132° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 526.83 km |
| Perigee altitude | 506.249 km |
| Semi-major axis | 6,894.676 km |
| Eccentricity | 0.0014925 |
| Inclination | 97.4754° |
| RAAN | 59.8292° |
| Arg. of periapsis | 173.8066° |
| True anomaly | 186.31656° |
| Mean anomaly | 186.3354° |
| Eccentric anomaly | 186.32598° |
| Mean motion | 3.79116 °/min |
| BSTAR | 0.00034977 |
| Orbital period | 94.96 mins |
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Other satellites on launch #205 in the year 2024 (2024-11-11 UTC)
OBJECT P 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-14 04:12:11.422Z | 106.436° ESE | 2024-12-14 04:14:11.422Z | 66.632° ENE | 19.445° | 2024-12-14 04:16:11.422Z | 28.743° NE |
| 5 mins | 2024-12-14 05:46:11.422Z | 222.523° SW | 2024-12-14 05:48:11.422Z | 267.459° W | 22.865° | 2024-12-14 05:51:11.422Z | 320.563° NNW |
| 4 mins | 2024-12-14 17:19:11.422Z | 59.858° ENE | 2024-12-14 17:20:11.422Z | 86.884° E | 26.338° | 2024-12-14 17:23:11.422Z | 154.774° SSE |
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