OBJECT P, 61907
Orbit data source: Space-Track
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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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: 2 days ago
TLE from 2 days ago
0 OBJECT P
1 61907U 24205P 26078.36136404 .00004047 00000-0 20768-3 0 9997
2 61907 97.4192 152.7676 0012563 13.9066 346.2511 15.17022858 74713Epoch: 2026-03-19T08:40Z
TLE epoch observation values (Epoch: 2026-03-19T08:40:21.853Z)
Latitude
0°
Longitude
-154.23534°
Altitude
509.517 km
Speed
7.614 km/s
True Right ascension
10h 11m 04s
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
11:43:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.47 km
Perigee altitude
503.159 km
Semi-major axis
6,889.952 km
Eccentricity
0.00126
Inclination
97.4192°
RAAN
152.7676°
Arg. of periapsis
13.9066°
True anomaly
346.21683°
Mean anomaly
346.2511°
Eccentric anomaly
346.23397°
Mean motion
3.79506 °/min
Orbital period
94.86 mins
BSTAR
0.00020768
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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 | 2026-03-21 18:14:16.643Z | 341.483° N | 2026-03-21 18:16:16.643Z | 282.403° WNW | 31.913° | 2026-03-21 18:19:16.643Z | 220.415° SW |
| 5 mins | 2026-03-22 04:53:16.643Z | 161.402° S | 2026-03-22 04:55:16.643Z | 61.597° ENE | 44.599° | 2026-03-22 04:58:16.643Z | 350.754° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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