OBJECT L, 64886
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 L, 64886 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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64886 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Civil Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.945 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 L
1 64886U 25155L 26025.62614522 .00040625 00000-0 12972-2 0 9993
2 64886 97.4340 354.7381 0006063 336.1883 23.9077 15.32345568 59036Epoch: 2026-01-25T15:01Z
TLE epoch observation values (Epoch: 2026-01-25T15:01:38.947Z)
Latitude
-0.00009°
Longitude
4.39228°
Altitude
468.127 km
Speed
7.634 km/s
True Right ascension
23h 38m 57s
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
22:01:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.916 km
Perigee altitude
461.617 km
Semi-major axis
6,843.904 km
Eccentricity
0.00061
Inclination
97.434°
RAAN
354.7381°
Arg. of periapsis
336.1883°
True anomaly
23.93588°
Mean anomaly
23.9077°
Eccentric anomaly
23.92179°
Mean motion
3.83343 °/min
Orbital period
93.91 mins
BSTAR
0.0012972
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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 L 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-01-25 21:25:36.796Z | 140.259° SSE | 2026-01-25 21:28:36.796Z | 72.874° E | 31.12° | 2026-01-25 21:31:36.796Z | 6.296° NNE |
| 5 mins | 2026-01-26 10:24:36.796Z | 32.67° NE | 2026-01-26 10:26:36.796Z | 96.297° ESE | 36.734° | 2026-01-26 10:29:36.796Z | 173.471° S |
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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