SL-16 DEB, 39850

Orbit data source: Space-Track

SL-16 DEB, 39850 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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Iframe URL

https://www.satcat.com/sats-embedded/39850?theme=dark&initialShowStats=false

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Identifier

39850, 1992-093LC

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: 3 days ago

TLE from 3 days ago

0 SL-16 DEB
1 39850U 92093LC  25347.18307368  .00001267  00000-0  74624-3 0  9997
2 39850  71.3348 149.6257 0091764 327.3663  32.1806 14.07694309310157

Epoch: 2025-12-13T04:23Z

TLE epoch observation values (Epoch: 2025-12-13T04:23:37.565Z)

Latitude

-0.00006°

Longitude

1.60515°

Altitude

813.581 km

Speed

7.475 km/s

True Right ascension

09h 58m 30s

True Declination

0° 00' 00"

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

15:11:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

931.639 km

Perigee altitude

798.704 km

Semi-major axis

7,243.309 km

Eccentricity

0.00918

Inclination

71.3348°

RAAN

149.6257°

Arg. of periapsis

327.3663°

True anomaly

32.74612°

Mean anomaly

32.1806°

Eccentric anomaly

32.46281°

Mean motion

3.52077 °/min

Orbital period

102.25 mins

BSTAR

0.00074624

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

SL-16 DEB, 39862

SL-16 DEB, 22546 (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.
7 mins	2025-12-15 20:02:14.010Z	13.203° NNE	2025-12-15 20:05:14.010Z	43.4° NE	15.255°	2025-12-15 20:09:14.010Z	84.844° E
11 mins	2025-12-15 21:46:14.010Z	337.811° N	2025-12-15 21:51:14.010Z	130.366° SE	44.972°	2025-12-15 21:57:14.010Z	158.649° S
8 mins	2025-12-16 10:58:14.010Z	153.92° SSE	2025-12-16 11:01:14.010Z	112.199° ESE	27.014°	2025-12-16 11:06:14.010Z	44.958° NE
9 mins	2025-12-16 12:42:14.010Z	241.724° WSW	2025-12-16 12:46:14.010Z	303.107° NW	30.508°	2025-12-16 12:51:14.010Z	6.167° 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, 39850 on other resources

View SL-16 DEB, 39850 on Heavens-Above

View SL-16 DEB, 39850 on Keep Track

View SL-16 DEB, 39850 on Celestrak

View SL-16 DEB, 39850 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, 39850

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-12-13T04:23:37.565Z)

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, 39850 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago