SL-16 DEB, 20626

Orbit data source: Space-Track

SL-16 DEB, 20626 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
20626, 1990-046C
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
SEP MOTOR COVER, Unknown motor
Mass
~0 kg wet, ~1 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
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 SL-16 DEB
1 20626U 90046C   25347.00726414  .00000087  00000-0  12039-3 0  9993
2 20626  71.0146 210.7204 0204367  48.0729  67.9433 13.72920874780544
Epoch: 2025-12-13T00:10Z
TLE epoch observation values (Epoch: 2025-12-13T00:10:27.621Z)
Latitude
56.54973°
Longitude
-85.03702°
Altitude
944.136 km
Speed
7.412 km/s
True Right ascension
23h 58m 04s
True Declination
56° 23' 43"
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
05:23:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,137.587 km
Perigee altitude
836.547 km
Semi-major axis
7,365.204 km
Eccentricity
0.02044
Inclination
71.0146°
RAAN
210.7204°
Arg. of periapsis
48.0729°
True anomaly
70.13426°
Mean anomaly
67.9433°
Eccentric anomaly
69.03673°
Mean motion
3.43373 °/min
Orbital period
104.84 mins
BSTAR
0.00012039
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Other satellites on launch #46 in the year 1990 (1990-05-22 UTC)

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