SL-16 DEB, 22805

Orbit data source: Space-Track

SL-16 DEB, 22805 is space debris in LEO originally from a launch on Thu, 16 Sep 1993 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
22805, 1993-059D
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)
1993-09-16 (33 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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 SL-16 DEB
1 22805U 93059D   26171.41862066  .00000080  00000-0  11821-3 0  9997
2 22805  70.9715 222.1290 0213087 199.0201 184.3113 13.70732598637809
Epoch: 2026-06-20T10:02Z
TLE epoch observation values (Epoch: 2026-06-20T10:02:48.825Z)
Latitude
21.84061°
Longitude
170.69684°
Altitude
1,155.802 km
Speed
7.2 km/s
True Right ascension
15h 20m 08s
True Declination
21° 43' 42"
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
00:51:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,152.022 km
Perigee altitude
837.802 km
Semi-major axis
7,373.049 km
Eccentricity
0.02131
Inclination
70.9715°
RAAN
222.129°
Arg. of periapsis
199.0201°
True anomaly
184.13249°
Mean anomaly
184.3113°
Eccentric anomaly
184.22143°
Mean motion
3.42825 °/min
Orbital period
105.01 mins
BSTAR
0.00011821
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