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 URL

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

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ISO8601 Format

Identifier

24302, 1996-051F

Orbit

LEO

Country

CIS

Related business

Russian Space Forces (RU)

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

CONE, 0.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago

0 SL-16 DEB
1 24302U 96051F   26318.81661687  .00000071  00000-0  10839-3 0  9997
2 24302  70.9847 251.1270 0205660  32.5128 358.4717 13.71209604510246

Epoch: 2026-11-14T19:35Z

TLE epoch observation values (Epoch: 2026-11-14T19:35:55.697Z)

Latitude

29.12304°

Longitude

-85.76109°

Altitude

846.687 km

Speed

7.508 km/s

True Right ascension

17h 28m 32s

True Declination

28° 58' 44"

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

01:42:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,144.799 km

Perigee altitude

841.601 km

Semi-major axis

7,371.337 km

Eccentricity

0.02057

Inclination

70.9847°

RAAN

251.127°

Arg. of periapsis

32.5128°

True anomaly

358.40719°

Mean anomaly

358.4717°

Eccentric anomaly

358.43961°

Mean motion

3.42944 °/min

Orbital period

104.97 mins

BSTAR

0.00010839

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

SL-16 DEB, 36030 (Decayed)

SL-16 DEB, 24875 (Decayed)

SL-16 DEB, 48078

SL-16 DEB, 24879 (Decayed)

SL-16 DEB, 36031 (Decayed)

SL-16 DEB, 25423 (Decayed)

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SL-16 DEB Visibility forecast

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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.
12 mins	2026-11-15 06:30:30.807Z	344.018° N	2026-11-15 06:36:30.807Z	85.212° E	63.818°	2026-11-15 06:42:30.807Z	146.04° SSE
8 mins	2026-11-15 08:19:30.807Z	297.688° NW	2026-11-15 08:23:30.807Z	254.345° W	20.74°	2026-11-15 08:27:30.807Z	216.982° SW
8 mins	2026-11-15 20:05:30.807Z	154.278° SSE	2026-11-15 20:08:30.807Z	112.156° ESE	30.522°	2026-11-15 20:13:30.807Z	45.046° ENE
8 mins	2026-11-15 21:52:30.807Z	245.037° WSW	2026-11-15 21:56:30.807Z	308.639° NW	34.333°	2026-11-15 22:00:30.807Z	2.072° NNE

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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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

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

SL-16 DEB, 24302

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-11-14T19:35:55.697Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

SL-16 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 DEB, 24302 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago