SL-16 R/B, 20625

Orbit data source: Space-Track

SL-16 R/B, 20625 is space debris in LEO originally from a launch on Tue, 22 May 1990 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
20625, 1990-046B
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
11S772, Unknown motor
Mass
9,000 kg wet, 9,000 kg dry
Launch date (UTC)
1990-05-22 (35 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 5.2 m
Radar Cross Section
37.829 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 SL-16 R/B
1 20625U 90046B   25300.51282130  .00000204  00000-0  12965-3 0  9998
2 20625  71.0000 217.5990 0013057 155.3569 204.8180 14.14991024829555
Epoch: 2025-10-27T12:18Z
TLE epoch observation values (Epoch: 2025-10-27T12:18:27.760Z)
Latitude
-0.00003°
Longitude
-3.13027°
Altitude
853.303 km
Speed
7.422 km/s
True Right ascension
14h 30m 23s
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
15:50:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
849.693 km
Perigee altitude
830.843 km
Semi-major axis
7,218.405 km
Eccentricity
0.00131
Inclination
71°
RAAN
217.599°
Arg. of periapsis
155.3569°
True anomaly
204.75529°
Mean anomaly
204.818°
Eccentric anomaly
204.78664°
Mean motion
3.53901 °/min
Orbital period
101.72 mins
BSTAR
0.00012965
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Other satellites on launch #46 in the year 1990 (1990-05-22 UTC)

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