OBJECT P, 64889
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 P, 64889 is a satellite in SSO that was launched on Fri, 25 Jul 2025 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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64889 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 OBJECT P
1 64889U 25155P 25338.70282036 .00012104 00000-0 50141-3 0 9994
2 64889 97.4348 302.4327 0008909 131.4592 228.7412 15.24025133 51068Epoch: 2025-12-04T16:52Z
TLE epoch observation values (Epoch: 2025-12-04T16:52:03.679Z)
Latitude
0.00003°
Longitude
-24.3381°
Altitude
500.851 km
Speed
7.612 km/s
True Right ascension
20h 09m 43s
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
08:55:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.795 km
Perigee altitude
484.557 km
Semi-major axis
6,868.813 km
Eccentricity
0.00089
Inclination
97.4348°
RAAN
302.4327°
Arg. of periapsis
131.4592°
True anomaly
228.66451°
Mean anomaly
228.7412°
Eccentric anomaly
228.70285°
Mean motion
3.81259 °/min
Orbital period
94.42 mins
BSTAR
0.00050141
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Other satellites on launch #155 in the year 2025 (2025-07-25 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 | 2025-12-05 21:22:22.686Z | 136° SSE | 2025-12-05 21:24:22.686Z | 91.378° ESE | 31.549° | 2025-12-05 21:27:22.686Z | 9.072° NNE |
| 5 mins | 2025-12-06 10:25:22.686Z | 31.862° NE | 2025-12-06 10:27:22.686Z | 129.86° SE | 39.081° | 2025-12-06 10:30:22.686Z | 180.138° SSW |
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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