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 (36 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: 20 hours ago

TLE from 20 hours ago
0 SL-16 R/B
1 20625U 90046B   25348.79598740 -.00000160  00000-0 -58217-4 0  9991
2 20625  70.9990 116.2031 0011854  69.4266 290.8127 14.15000952836381
Epoch: 2025-12-14T19:06Z
TLE epoch observation values (Epoch: 2025-12-14T19:06:13.311Z)
Latitude
-0.00003°
Longitude
105.94386°
Altitude
841.676 km
Speed
7.434 km/s
True Right ascension
07h 44m 48s
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
13:26:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
848.791 km
Perigee altitude
831.677 km
Semi-major axis
7,218.371 km
Eccentricity
0.00119
Inclination
70.999°
RAAN
116.2031°
Arg. of periapsis
69.4266°
True anomaly
290.68566°
Mean anomaly
290.8127°
Eccentric anomaly
290.74919°
Mean motion
3.53903 °/min
Orbital period
101.72 mins
BSTAR
-0.000058217
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Other satellites on launch #46 in the year 1990 (1990-05-22 UTC)

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