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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Iframe URL

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 (34 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.051 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  26304.61964670  .00000071  00000-0  10582-3 0  9993
2 39902  71.0066   3.0101 0192109 323.3449 190.5620 13.74627007622134

Epoch: 2026-10-31T14:52Z

TLE epoch observation values (Epoch: 2026-10-31T14:52:17.474Z)

Latitude

24.97883°

Longitude

-89.16523°

Altitude

1,124.605 km

Speed

7.223 km/s

True Right ascension

11h 35m 19s

True Declination

24° 51' 14"

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

14:04:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,122.344 km

Perigee altitude

839.594 km

Semi-major axis

7,359.106 km

Eccentricity

0.01921

Inclination

71.0066°

RAAN

3.0101°

Arg. of periapsis

323.3449°

True anomaly

190.1678°

Mean anomaly

190.562°

Eccentric anomaly

190.36398°

Mean motion

3.438 °/min

Orbital period

104.71 mins

BSTAR

0.00010582

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

SL-16 DEB, 42243 (Decayed)

SL-16 DEB, 22645

SL-16 DEB, 39905

SL-16 DEB, 22602

SL-16 DEB, 39897 (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.
11 mins	2026-11-02 04:38:33.915Z	176.319° S	2026-11-02 04:43:33.915Z	115.618° SE	46.813°	2026-11-02 04:49:33.915Z	35.36° NE
9 mins	2026-11-02 06:27:33.915Z	256.933° W	2026-11-02 06:31:33.915Z	309.902° NW	28.931°	2026-11-02 06:36:33.915Z	2.927° NNE
11 mins	2026-11-02 13:49:33.915Z	358.183° N	2026-11-02 13:54:33.915Z	52.49° ENE	33.799°	2026-11-02 14:00:33.915Z	116.778° SE
12 mins	2026-11-02 15:36:33.915Z	322.882° NNW	2026-11-02 15:42:33.915Z	244.717° WSW	48.543°	2026-11-02 15:48:33.915Z	183.411° 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: 2026-10-31T14:52:17.474Z)

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