SL-16 DEB, 39305

Orbit data source: Space-Track

SL-16 DEB, 39305 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/39305?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39305, 1992-093JW

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: 2 days ago

TLE from 2 days ago

0 SL-16 DEB
1 39305U 92093JW  26080.98762427  .00000188  00000-0  14694-3 0  9998
2 39305  70.9620 180.2645 0090233 137.3170 223.5002 14.02386426245013

Epoch: 2026-03-21T23:42Z

TLE epoch observation values (Epoch: 2026-03-21T23:42:10.736Z)

Latitude

-0.0001°

Longitude

5.21928°

Altitude

935.754 km

Speed

7.36 km/s

True Right ascension

12h 01m 03s

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

16:44:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

949.008 km

Perigee altitude

817.96 km

Semi-major axis

7,261.621 km

Eccentricity

0.00902

Inclination

70.962°

RAAN

180.2645°

Arg. of periapsis

137.317°

True anomaly

222.79424°

Mean anomaly

223.5002°

Eccentric anomaly

223.14664°

Mean motion

3.50746 °/min

Orbital period

102.64 mins

BSTAR

0.00014694

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

SL-16 DEB, 22483 (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.
5 mins	2026-03-24 15:35:42.243Z	18.337° NNE	2026-03-24 15:38:42.243Z	52.095° ENE	13.579°	2026-03-24 15:40:42.243Z	74.674° E
9 mins	2026-03-24 17:19:42.243Z	336.488° NNW	2026-03-24 17:23:42.243Z	332.031° NNW	44.116°	2026-03-24 17:28:42.243Z	159.12° S
8 mins	2026-03-25 06:34:42.243Z	157.09° SSE	2026-03-25 06:38:42.243Z	95.726° ESE	28.92°	2026-03-25 06:42:42.243Z	45.536° ENE
8 mins	2026-03-25 08:19:42.243Z	247.011° WSW	2026-03-25 08:23:42.243Z	311.552° NW	29.493°	2026-03-25 08:27:42.243Z	2.547° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out SL-16 DEB, 39305 on other resources

View SL-16 DEB, 39305 on Heavens-Above

View SL-16 DEB, 39305 on Keep Track

View SL-16 DEB, 39305 on Celestrak

View SL-16 DEB, 39305 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, 39305

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-03-21T23:42:10.736Z)

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, 39305 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago