SL-3 R/B, 12904

Orbit data source: Space-Track

SL-3 R/B, 12904 is space debris in LEO originally from a launch on Tue, 13 Oct 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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Identifier
12904, 1981-103B
Orbit
LEO
Last TLE update
10 hours ago
Origin
Manufacturer
Progress
Mission
Spacecraft
Bus & Motor
BLOK-E, Unknown motor
Mass
1,440 kg wet, 1,440 kg dry
Launch date (UTC)
1981-10-13 (44 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.9 m
Radar Cross Section
10.414 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 10 hours ago
0 SL-3 R/B
1 12904U 81103B   25197.86501404  .00002924  00000-0  14063-3 0  9995
2 12904  81.1612 129.3943 0018526  20.0526 340.1427 15.18337194937412
Epoch: 2025-07-16T20:45Z
TLE epoch observation values (Epoch: 2025-07-16T20:45:37.213Z)
Latitude
-0.00004°
Longitude
-116.94981°
Altitude
501.905 km
Speed
7.62 km/s
True Right ascension
08h 37m 34s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
29.73746°
Longitude
-112.3495°
Altitude
502.145 km
Speed
7.623 km/s
Apparent Right ascension
08h 05m 32s
Apparent Declination
-3° 40' 03"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:03:44
Azimuth
334.923° NNW
Elevation
-51.151°
Doppler factor
1
Orbital elements
Apogee altitude
520.658 km
Perigee altitude
495.144 km
Semi-major axis
6,886.038 km
Eccentricity
0.00185
Inclination
81.1612°
RAAN
129.3943°
Arg. of periapsis
20.0526°
True anomaly
Unknown
Mean anomaly
340.1427°
Eccentric anomaly
Unknown
Mean motion
3.7983 °/min
Orbital period
94.78 mins
BSTAR
0.00014063
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Other satellites on launch #103 in the year 1981 (1981-10-13 UTC)
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