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

13 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 13 hours ago

0 SL-16 DEB
1 24302U 96051F   25129.30542130  .00000102  00000-0  13792-3 0  9997
2 24302  70.9847 254.9328 0205099  95.6053 291.2463 13.71073977434232

Epoch: 2025-05-09T07:19Z

Definitive object data (Epoch: 2025-05-09T07:19:48.4Z)

Latitude

23.24437°

Longitude

-73.91477°

Altitude

945.892 km

Speed

7.407 km/s

True Right ascension

17h 33m 36s

True Declination

23° 07' 23"

Sunlit

Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude

-71.06629°

Longitude

-175.16408°

Altitude

1,172.165 km

Speed

7.192 km/s

Apparent Right ascension

15h 08m 56s

Apparent Declination

-64° 14' 58"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:57:07

Azimuth

155.943° SSE

Elevation

-61.012°

Doppler factor

Orbital elements

Apogee altitude

1,144.882 km

Perigee altitude

842.491 km

Semi-major axis

7,371.823 km

Eccentricity

0.0205099

Inclination

70.9847°

RAAN

254.9328°

Arg. of periapsis

95.6053°

True anomaly

289.0358°

Mean anomaly

291.2463°

Eccentric anomaly

290.14305°

Mean motion

3.42911 °/min

BSTAR

0.00013792

Orbital period

104.98 mins

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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.
11 mins	2025-05-10 09:34:56.262Z	198.814° SSW	2025-05-10 09:40:56.262Z	68.162° E	44.743°	2025-05-10 09:45:56.262Z	24.639° NE
5 mins	2025-05-10 11:26:56.262Z	288.454° WNW	2025-05-10 11:28:56.262Z	311.463° NW	14.974°	2025-05-10 11:31:56.262Z	344.277° N
9 mins	2025-05-10 18:47:56.262Z	353.967° N	2025-05-10 18:51:56.262Z	63.096° ENE	36.899°	2025-05-10 18:56:56.262Z	134.542° SE
7 mins	2025-05-10 20:35:56.262Z	297.243° NW	2025-05-10 20:38:56.262Z	258.549° W	21.148°	2025-05-10 20:42:56.262Z	212.389° SW

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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