SL-16 DEB, 22577

Orbit data source: Space-Track

SL-16 DEB, 22577 is space debris in LEO originally from a launch on Fri, 26 Mar 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
22577, 1993-016E
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)
1993-03-26 (33 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.6 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 SL-16 DEB
1 22577U 93016E   26083.38421316  .00000140  00000-0  53010-4 0  9997
2 22577  71.0401 150.9889 0117140 211.7020 227.5722 14.43888441736801
Epoch: 2026-03-24T09:13Z
TLE epoch observation values (Epoch: 2026-03-24T09:13:16.017Z)
Latitude
67.92953°
Longitude
-111.75156°
Altitude
813.722 km
Speed
7.423 km/s
True Right ascension
13h 53m 42s
True Declination
67° 48' 38"
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
00:25:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
826.996 km
Perigee altitude
660.148 km
Semi-major axis
7,121.709 km
Eccentricity
0.01171
Inclination
71.0401°
RAAN
150.9889°
Arg. of periapsis
211.702°
True anomaly
226.59114°
Mean anomaly
227.5722°
Eccentric anomaly
227.0807°
Mean motion
3.61133 °/min
Orbital period
99.69 mins
BSTAR
0.00005301
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