SL-16 DEB, 39886

Orbit data source: Space-Track

SL-16 DEB, 39886 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/39886?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39886, 1993-016BL

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: 4 days ago

TLE from 4 days ago

0 SL-16 DEB
1 39886U 93016BL  25350.34348335  .00003610  00000-0  51078-3 0  9995
2 39886  71.0087  13.9714 0045271 164.4592 195.7966 14.77131928615271

Epoch: 2025-12-16T08:14Z

TLE epoch observation values (Epoch: 2025-12-16T08:14:36.961Z)

Latitude

-0.00002°

Longitude

165.08834°

Altitude

671.443 km

Speed

7.505 km/s

True Right ascension

00h 55m 53s

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

20:13:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

668.01 km

Perigee altitude

604.5 km

Semi-major axis

7,014.392 km

Eccentricity

0.00453

Inclination

71.0087°

RAAN

13.9714°

Arg. of periapsis

164.4592°

True anomaly

195.65614°

Mean anomaly

195.7966°

Eccentric anomaly

195.7263°

Mean motion

3.69452 °/min

Orbital period

97.44 mins

BSTAR

0.00051078

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

SL-16 DEB, 29099 (Decayed)

SL-16 R/B, 22566

SL-16 DEB, 39897 (Decayed)

SL-16 DEB, 42246

SL-16 DEB, 39869 (Decayed)

SL-16 DEB, 42238 (Decayed)

SL-16 DEB, 39910 (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.
7 mins	2025-12-20 01:44:56.264Z	166.607° S	2025-12-20 01:48:56.264Z	104.22° ESE	27.57°	2025-12-20 01:51:56.264Z	50.829° ENE
6 mins	2025-12-20 03:25:56.264Z	256.968° W	2025-12-20 03:28:56.264Z	311.507° NW	23.187°	2025-12-20 03:31:56.264Z	355.763° N
7 mins	2025-12-20 11:56:56.264Z	346.794° N	2025-12-20 11:59:56.264Z	61.886° ENE	42.043°	2025-12-20 12:03:56.264Z	146.867° SSE

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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, 39886 on other resources

View SL-16 DEB, 39886 on Heavens-Above

View SL-16 DEB, 39886 on Keep Track

View SL-16 DEB, 39886 on Celestrak

View SL-16 DEB, 39886 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, 39886

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2025-12-16T08:14:36.961Z)

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, 39886 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 4 days ago