SL-16 DEB, 39848

Orbit data source: Space-Track

SL-16 DEB, 39848 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/39848?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39848, 1992-093LA

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 (34 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.050 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 39848U 92093LA  26302.75876732  .00058475  00000-0  25419-2 0  9995
2 39848  71.2025 114.3677 0014583 310.3941  49.5965 15.21881137645484

Epoch: 2026-10-29T18:12Z

TLE epoch observation values (Epoch: 2026-10-29T18:12:37.496Z)

Latitude

-0.00005°

Longitude

163.12286°

Altitude

496.206 km

Speed

7.62 km/s

True Right ascension

07h 37m 28s

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

06:08:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

507.995 km

Perigee altitude

487.94 km

Semi-major axis

6,876.104 km

Eccentricity

0.00146

Inclination

71.2025°

RAAN

114.3677°

Arg. of periapsis

310.3941°

True anomaly

49.7239°

Mean anomaly

49.5965°

Eccentric anomaly

49.66019°

Mean motion

3.80653 °/min

Orbital period

94.57 mins

BSTAR

0.0025419

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

SL-16 DEB, 22389 (Decayed)

SL-16 DEB, 44574

SL-16 DEB, 39707

SL-16 DEB, 22360 (Decayed)

SL-16 DEB, 39866 (Decayed)

SL-16 DEB, 22378 (Decayed)

SL-16 DEB, 22510 (Decayed)

SL-16 DEB, 22479 (Decayed)

SL-16 DEB, 22411 (Decayed)

SL-16 DEB, 22412 (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.
6 mins	2026-11-03 11:54:28.848Z	192.023° SSW	2026-11-03 11:57:28.848Z	85.246° E	67.938°	2026-11-03 12:00:28.848Z	28.434° NE
6 mins	2026-11-03 21:47:28.848Z	336.271° NNW	2026-11-03 21:50:28.848Z	169.893° S	73.802°	2026-11-03 21:53:28.848Z	159.786° 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, 39848 on other resources

View SL-16 DEB, 39848 on Heavens-Above

View SL-16 DEB, 39848 on Keep Track

View SL-16 DEB, 39848 on Celestrak

View SL-16 DEB, 39848 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, 39848

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: 2026-10-29T18:12:37.496Z)

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, 39848 on other resources

Documentation

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