SL-16 DEB, 20627

Orbit data source: Space-Track

SL-16 DEB, 20627 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
20627, 1990-046D
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, 0.2 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SL-16 DEB
1 20627U 90046D   26093.20550012  .00000274  00000-0  30214-3 0  9997
2 20627  70.9770  15.8348 0210898  35.6621 128.1085 13.70983960793380
Epoch: 2026-04-03T04:55Z
TLE epoch observation values (Epoch: 2026-04-03T04:55:55.210Z)
Latitude
13.53507°
Longitude
-74.42467°
Altitude
1,095.637 km
Speed
7.257 km/s
True Right ascension
12h 44m 23s
True Declination
13° 27' 38"
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
13:17:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,149.487 km
Perigee altitude
838.533 km
Semi-major axis
7,372.147 km
Eccentricity
0.02109
Inclination
70.977°
RAAN
15.8348°
Arg. of periapsis
35.6621°
True anomaly
129.97928°
Mean anomaly
128.1085°
Eccentric anomaly
129.04695°
Mean motion
3.42888 °/min
Orbital period
104.99 mins
BSTAR
0.00030214
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Other satellites on launch #46 in the year 1990 (1990-05-22 UTC)

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