SL-16 DEB, 24302

Orbit data source: Space-Track

SL-16 DEB, 24302 is space debris in LEO originally from a launch on Wed, 04 Sep 1996 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
24302, 1996-051F
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)
1996-09-04 (30 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 24302U 96051F   26171.40365148  .00000050  00000-0  89502-4 0  9993
2 24302  70.9826 179.2746 0208947 241.3408 238.4891 13.71193344490030
Epoch: 2026-06-20T09:41Z
TLE epoch observation values (Epoch: 2026-06-20T09:41:15.487Z)
Latitude
56.84572°
Longitude
-86.32194°
Altitude
1,087.096 km
Speed
7.273 km/s
True Right ascension
21h 50m 26s
True Declination
56° 41' 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
02:18:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,147.281 km
Perigee altitude
839.235 km
Semi-major axis
7,371.395 km
Eccentricity
0.02089
Inclination
70.9826°
RAAN
179.2746°
Arg. of periapsis
241.3408°
True anomaly
236.47573°
Mean anomaly
238.4891°
Eccentric anomaly
237.47964°
Mean motion
3.4294 °/min
Orbital period
104.97 mins
BSTAR
0.000089502
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