SL-16 DEB, 39895

Orbit data source: Space-Track

SL-16 DEB, 39895 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/39895?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39895, 1993-016BV

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: 6 hours ago

TLE from 6 hours ago

0 SL-16 DEB
1 39895U 93016BV  26084.52598294  .00000468  00000-0  35104-3 0  9991
2 39895  70.9918   8.9276 0119382  78.7765 282.6739 13.96197058322245

Epoch: 2026-03-25T12:37Z

TLE epoch observation values (Epoch: 2026-03-25T12:37:24.926Z)

Latitude

0.00007°

Longitude

-3.41426°

Altitude

891.28 km

Speed

7.416 km/s

True Right ascension

00h 35m 42s

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

23:21:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

991.884 km

Perigee altitude

817.991 km

Semi-major axis

7,283.075 km

Eccentricity

0.01194

Inclination

70.9918°

RAAN

8.9276°

Arg. of periapsis

78.7765°

True anomaly

281.33495°

Mean anomaly

282.6739°

Eccentric anomaly

282.00485°

Mean motion

3.49197 °/min

Orbital period

103.09 mins

BSTAR

0.00035104

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

SL-16 DEB, 39909 (Decayed)

SL-16 DEB, 42238 (Decayed)

SL-16 DEB, 39886

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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.
10 mins	2026-03-25 19:36:17.527Z	169.946° S	2026-03-25 19:41:17.527Z	106.294° ESE	30.71°	2026-03-25 19:46:17.527Z	40.404° NE
8 mins	2026-03-25 21:23:17.527Z	250.89° W	2026-03-25 21:26:17.527Z	292.311° WNW	26.274°	2026-03-25 21:31:17.527Z	1.484° NNE
6 mins	2026-03-26 04:39:17.527Z	16.582° NNE	2026-03-26 04:42:17.527Z	54.606° ENE	18.761°	2026-03-26 04:45:17.527Z	90.964° ESE
9 mins	2026-03-26 06:24:17.527Z	325.732° NNW	2026-03-26 06:28:17.527Z	237.515° WSW	41.489°	2026-03-26 06:33:17.527Z	172.172° 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, 39895 on other resources

View SL-16 DEB, 39895 on Heavens-Above

View SL-16 DEB, 39895 on Keep Track

View SL-16 DEB, 39895 on Celestrak

View SL-16 DEB, 39895 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, 39895

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-03-25T12:37:24.926Z)

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, 39895 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago