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: 12 hours ago

TLE from 12 hours ago
0 SL-16 DEB
1 22577U 93016E   26137.68944543  .00000062  00000-0  31882-4 0  9998
2 22577  71.0414  31.6496 0113900 124.4132 268.2113 14.43904517744648
Epoch: 2026-05-17T16:32Z
TLE epoch observation values (Epoch: 2026-05-17T16:32:48.085Z)
Latitude
29.50694°
Longitude
-80.78965°
Altitude
752.267 km
Speed
7.48 km/s
True Right ascension
02h 51m 11s
True Declination
29° 21' 35"
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
13:24:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.635 km
Perigee altitude
662.403 km
Semi-major axis
7,121.656 km
Eccentricity
0.01139
Inclination
71.0414°
RAAN
31.6496°
Arg. of periapsis
124.4132°
True anomaly
266.90743°
Mean anomaly
268.2113°
Eccentric anomaly
267.55929°
Mean motion
3.61137 °/min
Orbital period
99.69 mins
BSTAR
0.000031882
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