SL-16 DEB, 39902

Orbit data source: Space-Track

SL-16 DEB, 39902 is space debris in LEO originally from a launch on Fri, 26 Mar 1993 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/39902?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39902, 1993-016CC

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1993-03-26 (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: 1 day ago

TLE from 1 day ago

0 SL-16 DEB
1 39902U 93016CC  26082.74973443  .00000122  00000-0  15347-3 0  9999
2 39902  71.0020  78.7228 0192607 279.2188 257.4931 13.74556759591649

Epoch: 2026-03-23T17:59Z

TLE epoch observation values (Epoch: 2026-03-23T17:59:37.054Z)

Latitude

5.06073°

Longitude

165.843°

Altitude

1,018.393 km

Speed

7.327 km/s

True Right ascension

17h 07m 56s

True Declination

5° 01' 54"

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

02:02:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,122.967 km

Perigee altitude

839.474 km

Semi-major axis

7,359.357 km

Eccentricity

0.01926

Inclination

71.002°

RAAN

78.7228°

Arg. of periapsis

279.2188°

True anomaly

255.35004°

Mean anomaly

257.4931°

Eccentric anomaly

256.42039°

Mean motion

3.43782 °/min

Orbital period

104.72 mins

BSTAR

0.00015347

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Other satellites on launch #16 in the year 1993 (1993-03-26 UTC)

SL-16 DEB *, 29101 (Decayed)

SL-16 DEB, 39896 (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.
13 mins	2026-03-25 00:39:41.699Z	191.245° SSW	2026-03-25 00:45:41.699Z	129.143° SE	43.149°	2026-03-25 00:52:41.699Z	27.631° NE
8 mins	2026-03-25 02:30:41.699Z	273.301° WNW	2026-03-25 02:33:41.699Z	307.018° NW	21.709°	2026-03-25 02:38:41.699Z	357.078° N
11 mins	2026-03-25 09:52:41.699Z	354.848° N	2026-03-25 09:57:41.699Z	62.818° ENE	35.429°	2026-03-25 10:03:41.699Z	130.454° SE
10 mins	2026-03-25 11:39:41.699Z	313.211° NW	2026-03-25 11:44:41.699Z	255.87° W	28.825°	2026-03-25 11:49:41.699Z	200.664° SSW

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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, 39902 on other resources

View SL-16 DEB, 39902 on Heavens-Above

View SL-16 DEB, 39902 on Keep Track

View SL-16 DEB, 39902 on Celestrak

View SL-16 DEB, 39902 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, 39902

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: 2026-03-23T17:59:37.054Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #16 in the year 1993 (1993-03-26 UTC)

SL-16 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 DEB, 39902 on other resources

Documentation

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