SL-3 R/B, 12586

Orbit data source: Space-Track

SL-3 R/B, 12586 is space debris in SSO originally from a launch on Fri, 10 Jul 1981 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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
12586, 1981-065B
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
Progress
Mission
Spacecraft
Bus & Motor
BLOK-E, Unknown motor
Mass
1,440 kg wet, 1,440 kg dry
Launch date (UTC)
1981-07-10 (44 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 SL-3 R/B
1 12586U 81065B   25328.05853469  .00008972  00000-0  29902-3 0  9993
2 12586  97.6486   1.9429 0012966  24.0710 336.1134 15.31264662418782
Epoch: 2025-11-24T01:24Z
TLE epoch observation values (Epoch: 2025-11-24T01:24:17.397Z)
Latitude
Longitude
-82.39354°
Altitude
467.015 km
Speed
7.637 km/s
True Right ascension
00h 07m 46s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:53:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.877 km
Perigee altitude
460.121 km
Semi-major axis
6,847.136 km
Eccentricity
0.0013
Inclination
97.6486°
RAAN
1.9429°
Arg. of periapsis
24.071°
True anomaly
336.05315°
Mean anomaly
336.1134°
Eccentric anomaly
336.08328°
Mean motion
3.83071 °/min
Orbital period
93.98 mins
BSTAR
0.00029902
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Other satellites on launch #65 in the year 1981 (1981-07-10 UTC)

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