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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<iframe src="https://www.satcat.com/sats-embedded/24302?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/24302?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

24302, 1996-051F

Orbit

LEO

Last TLE update

9 hours ago

Origin

Russian Space Forces (CIS)

Manufacturer

Yuzhnoe

Mission

Spacecraft

Bus & Motor

SEP MOTOR COVER, Unknown motor

Mass

~0 kg wet, ~1 kg dry

Launch date (UTC)

1996-09-04 (29 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 SL-16 DEB
1 24302U 96051F   25186.94666668  .00000070  00000-0  10844-3 0  9992
2 24302  70.9841 142.2935 0206531  13.6359  42.6455 13.71086856442137

Epoch: 2025-07-05T22:43Z

TLE epoch observation values (Epoch: 2025-07-05T22:43:12.001Z)

Latitude

53.34007°

Longitude

-95.25788°

Altitude

893.289 km

Speed

7.466 km/s

True Right ascension

11h 18m 52s

True Declination

53° 10' 42"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-13.97974°

Longitude

61.4456°

Altitude

1,153.144 km

Speed

7.201 km/s

Apparent Right ascension

00h 08m 16s

Apparent Declination

-59° 05' 25"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

20:06:39

Azimuth

151.447° SSE

Elevation

-20.851°

Doppler factor

Orbital elements

Apogee altitude

1,145.89 km

Perigee altitude

841.39 km

Semi-major axis

7,371.777 km

Eccentricity

0.02065

Inclination

70.9841°

RAAN

142.2935°

Arg. of periapsis

13.6359°

True anomaly

Unknown

Mean anomaly

42.6455°

Eccentric anomaly

Unknown

Mean motion

3.42914 °/min

Orbital period

104.98 mins

BSTAR

0.00010844

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Other satellites on launch #51 in the year 1996 (1996-09-04 UTC)

SL-16 DEB, 24875 (Decayed)

SL-16 DEB, 24879 (Decayed)

SL-16 DEB, 25423 (Decayed)

SL-16 DEB, 36030 (Decayed)

SL-16 DEB, 36031 (Decayed)

SL-16 DEB, 43354

SL-16 DEB, 48078

SL-16 DEB Visibility forecast

Observer location: undefined°, undefined°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
10 mins	2025-07-06 09:32:52.148Z	309.902° NW	2025-07-06 09:37:52.148Z	259.283° W	23.455°	2025-07-06 09:42:52.148Z	209.732° SW
7 mins	2025-07-06 21:20:52.148Z	141.327° SSE	2025-07-06 21:23:52.148Z	97.357° ESE	23.391°	2025-07-06 21:27:52.148Z	49.953° ENE
9 mins	2025-07-06 23:06:52.148Z	236.984° WSW	2025-07-06 23:10:52.148Z	304.139° NW	33.595°	2025-07-06 23:15:52.148Z	9.037° NNE
8 mins	2025-07-07 06:30:52.148Z	12.05° NNE	2025-07-07 06:34:52.148Z	55.871° ENE	20.479°	2025-07-07 06:38:52.148Z	95.291° ESE

Authenticating...

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Check out SL-16 DEB, 24302 on other resources

View SL-16 DEB, 24302 on Heavens-Above

View SL-16 DEB, 24302 on Keep Track

View SL-16 DEB, 24302 on Celestrak

View SL-16 DEB, 24302 on Gunter's Space Page

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