SL-8 R/B, 12508
Orbit data source: Space-Track
SL-8 R/B, 12508 is space debris in LEO originally from a launch on Thu, 04 Jun 1981 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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12508 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Omsk Av. Zav.
Mission
Spacecraft
Bus & Motor
S3, Unknown motor
Mass
1,434 kg wet, 1,434 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 SL-8 R/B
1 12508U 81053B 25286.58354841 .00000092 00000-0 78045-4 0 9993
2 12508 82.9593 50.5502 0036918 343.9124 16.0858 13.76612623233489Epoch: 2025-10-13T14:00Z
TLE epoch observation values (Epoch: 2025-10-13T14:00:18.582Z)
Latitude
0.00002°
Longitude
178.08854°
Altitude
952.744 km
Speed
7.388 km/s
True Right ascension
03h 22m 12s
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
16:17:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,000.211 km
Perigee altitude
945.933 km
Semi-major axis
7,351.209 km
Eccentricity
0.00369
Inclination
82.9593°
RAAN
50.5502°
Arg. of periapsis
343.9124°
True anomaly
16.20354°
Mean anomaly
16.0858°
Eccentric anomaly
16.14462°
Mean motion
3.44354 °/min
Orbital period
104.54 mins
BSTAR
0.000078045
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Other satellites on launch #53 in the year 1981 (1981-06-04 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.SL-8 R/B 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 | 2025-10-14 07:35:44.050Z | 111.139° ESE | 2025-10-14 07:38:44.050Z | 80.442° E | 14.708° | 2025-10-14 07:41:44.050Z | 50.034° ENE |
| 10 mins | 2025-10-14 09:18:44.050Z | 195.402° SSW | 2025-10-14 09:23:44.050Z | 311.183° NW | 43.205° | 2025-10-14 09:28:44.050Z | 2.197° NNE |
| 10 mins | 2025-10-14 20:15:44.050Z | 353.546° N | 2025-10-14 20:19:44.050Z | 358.096° N | 44.494° | 2025-10-14 20:25:44.050Z | 174.395° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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