SL-8 R/B, 22676

Orbit data source: Space-Track

SL-8 R/B, 22676 is space debris in LEO originally from a launch on Wed, 16 Jun 1993 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.

Loading next visibility...
Identifier
22676, 1993-036B
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Polyot
Mission
Spacecraft
Bus & Motor
S3, Unknown motor
Mass
1,434 kg wet, 1,434 kg dry
Launch date (UTC)
1993-06-16 (33 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.3 m
Radar Cross Section
14.646 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 SL-8 R/B
1 22676U 93036B   25356.87729646  .00000232  00000-0  90162-4 0  9993
2 22676  74.0414 249.7291 0019379 237.1546 122.7742 14.35218028701003
Epoch: 2025-12-22T21:03Z
TLE epoch observation values (Epoch: 2025-12-22T21:03:18.414Z)
Latitude
0.00007°
Longitude
-157.76669°
Altitude
784.476 km
Speed
7.458 km/s
True Right ascension
16h 38m 54s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
05:17:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
785.823 km
Perigee altitude
758.11 km
Semi-major axis
7,150.103 km
Eccentricity
0.00194
Inclination
74.0414°
RAAN
249.7291°
Arg. of periapsis
237.1546°
True anomaly
122.96067°
Mean anomaly
122.7742°
Eccentric anomaly
122.86746°
Mean motion
3.58984 °/min
Orbital period
100.28 mins
BSTAR
0.000090162

Documentation

Showing up to 5 results
|