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)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Defense Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
4.795 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OBJECT P
1 61907U 24205P 25298.88576750 .00008474 00000-0 42758-3 0 9990
2 61907 97.4401 11.0090 0014752 147.9941 212.2191 15.17269011 52801Epoch: 2025-10-25T21:15Z
TLE epoch observation values (Epoch: 2025-10-25T21:15:30.312Z)
Latitude
-0.00011°
Longitude
17.62283°
Altitude
525.792 km
Speed
7.595 km/s
True Right ascension
00h 44m 02s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:05:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.233 km
Perigee altitude
500.907 km
Semi-major axis
6,889.207 km
Eccentricity
0.00148
Inclination
97.4401°
RAAN
11.009°
Arg. of periapsis
147.9941°
True anomaly
212.12911°
Mean anomaly
212.2191°
Eccentric anomaly
212.17409°
Mean motion
3.79568 °/min
Orbital period
94.84 mins
BSTAR
0.00042758
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Other satellites on launch #205 in the year 2024 (2024-11-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT P Visibility forecast
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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 | 2025-10-26 05:18:42.089Z | 194.909° SSW | 2025-10-26 05:20:42.089Z | 255.848° W | 36.891° | 2025-10-26 05:23:42.089Z | 332.979° NNW |
| 4 mins | 2025-10-26 18:24:42.089Z | 333.269° NNW | 2025-10-26 18:26:42.089Z | 278.416° WNW | 26.546° | 2025-10-26 18:28:42.089Z | 234.745° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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