SL-16 DEB, 39300

Orbit data source: Space-Track

SL-16 DEB, 39300 is space debris in LEO originally from a launch on Fri, 25 Dec 1992 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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https://www.satcat.com/sats-embedded/39300?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39300, 1992-093JR

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1992-12-25 (33 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: 5 days ago

TLE from 5 days ago

0 SL-16 DEB
1 39300U 92093JR  25345.49563037  .00000502  00000-0  37504-3 0  9993
2 39300  71.1221  71.5978 0105221 213.4088 146.0359 13.96867996623727

Epoch: 2025-12-11T11:53Z

TLE epoch observation values (Epoch: 2025-12-11T11:53:42.463Z)

Latitude

-0.00004°

Longitude

172.72008°

Altitude

970.862 km

Speed

7.334 km/s

True Right ascension

04h 46m 23s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

18:31:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

979.2 km

Perigee altitude

825.983 km

Semi-major axis

7,280.728 km

Eccentricity

0.01052

Inclination

71.1221°

RAAN

71.5978°

Arg. of periapsis

213.4088°

True anomaly

146.70223°

Mean anomaly

146.0359°

Eccentric anomaly

146.36979°

Mean motion

3.49366 °/min

Orbital period

103.04 mins

BSTAR

0.00037504

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Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB, 22553 (Decayed)

SL-16 DEB, 22505 (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.
11 mins	2025-12-17 05:29:31.655Z	168.999° S	2025-12-17 05:34:31.655Z	111.173° ESE	32.371°	2025-12-17 05:40:31.655Z	38.339° NE
9 mins	2025-12-17 07:16:31.655Z	249.053° W	2025-12-17 07:20:31.655Z	306.899° NW	29.621°	2025-12-17 07:25:31.655Z	4.66° NNE
6 mins	2025-12-17 14:33:31.655Z	19.827° NNE	2025-12-17 14:36:31.655Z	57.807° ENE	18.767°	2025-12-17 14:39:31.655Z	92.29° ESE
10 mins	2025-12-17 16:17:31.655Z	328.917° NNW	2025-12-17 16:21:31.655Z	279.292° WNW	41.538°	2025-12-17 16:27:31.655Z	170.581° S

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out SL-16 DEB, 39300 on other resources

View SL-16 DEB, 39300 on Heavens-Above

View SL-16 DEB, 39300 on Keep Track

View SL-16 DEB, 39300 on Celestrak

View SL-16 DEB, 39300 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, 39300

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 days ago

TLE from 5 days ago

TLE epoch observation values (Epoch: 2025-12-11T11:53:42.463Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 DEB, 39300 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 days ago