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
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 SL-16 DEB
1 24302U 96051F   26094.08207800  .00000165  00000-0  19918-3 0  9991
2 24302  70.9863 330.4194 0207400 349.6712 159.7997 13.71175821479435
Epoch: 2026-04-04T01:58Z
TLE epoch observation values (Epoch: 2026-04-04T01:58:11.539Z)
Latitude
28.0073°
Longitude
-82.04237°
Altitude
1,142.15 km
Speed
7.213 km/s
True Right ascension
09h 19m 39s
True Declination
27° 52' 20"
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
18:42:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,146.205 km
Perigee altitude
840.437 km
Semi-major axis
7,371.458 km
Eccentricity
0.02074
Inclination
70.9863°
RAAN
330.4194°
Arg. of periapsis
349.6712°
True anomaly
160.60082°
Mean anomaly
159.7997°
Eccentric anomaly
160.20218°
Mean motion
3.42936 °/min
Orbital period
104.98 mins
BSTAR
0.00019918
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