SL-16 DEB, 39726

Orbit data source: Space-Track

SL-16 DEB, 39726 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/39726?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39726, 1992-093KS

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, 0.065 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 SL-16 DEB
1 39726U 92093KS  26312.11249609  .00000100  00000-0  10654-3 0  9996
2 39726  71.1593 350.6161 0119749 138.7671 253.4631 13.91382506637559

Epoch: 2026-11-08T02:41Z

TLE epoch observation values (Epoch: 2026-11-08T02:41:59.662Z)

Latitude

29.15454°

Longitude

-86.27541°

Altitude

952.734 km

Speed

7.365 km/s

True Right ascension

00h 06m 07s

True Declination

29° 00' 44"

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

02:18:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,009.137 km

Perigee altitude

834.307 km

Semi-major axis

7,299.859 km

Eccentricity

0.01197

Inclination

71.1593°

RAAN

350.6161°

Arg. of periapsis

138.7671°

True anomaly

252.15333°

Mean anomaly

253.4631°

Eccentric anomaly

252.80765°

Mean motion

3.47994 °/min

Orbital period

103.45 mins

BSTAR

0.00010654

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

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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.
4 mins	2026-11-09 11:53:41.622Z	24.043° NE	2026-11-09 11:55:41.622Z	45.368° ENE	12.27°	2026-11-09 11:57:41.622Z	67.033° ENE
9 mins	2026-11-09 13:38:41.622Z	341.632° N	2026-11-09 13:42:41.622Z	83.825° E	78.143°	2026-11-09 13:47:41.622Z	153.355° SSE
9 mins	2026-11-10 02:58:41.622Z	162.042° S	2026-11-10 03:02:41.622Z	113.594° SE	34.557°	2026-11-10 03:07:41.622Z	44.926° NE
9 mins	2026-11-10 04:44:41.622Z	242.276° WSW	2026-11-10 04:48:41.622Z	296.018° NW	35.845°	2026-11-10 04:53:41.622Z	3.485° 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, 39726 on other resources

View SL-16 DEB, 39726 on Heavens-Above

View SL-16 DEB, 39726 on Keep Track

View SL-16 DEB, 39726 on Celestrak

View SL-16 DEB, 39726 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, 39726

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-11-08T02:41:59.662Z)

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, 39726 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago