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: 1 day ago

TLE from 1 day ago

0 SL-16 DEB
1 39886U 93016BL  26254.25828149  .00002915  00000-0  39019-3 0  9993
2 39886  71.0042 108.3833 0043084  66.1921 294.3744 14.79739929655021

Epoch: 2026-09-11T06:11Z

TLE epoch observation values (Epoch: 2026-09-11T06:11:55.520Z)

Latitude

0.00002°

Longitude

25.11775°

Altitude

620.264 km

Speed

7.556 km/s

True Right ascension

07h 13m 31s

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

09:44:01

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

658.192 km

Perigee altitude

597.821 km

Semi-major axis

7,006.144 km

Eccentricity

0.00431

Inclination

71.0042°

RAAN

108.3833°

Arg. of periapsis

66.1921°

True anomaly

293.9237°

Mean anomaly

294.3744°

Eccentric anomaly

294.14915°

Mean motion

3.70105 °/min

Orbital period

97.27 mins

BSTAR

0.00039019

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

SL-16 DEB, 39899 (Decayed)

SL-16 DEB, 22579

SL-16 DEB, 22645

SL-16 DEB, 29099 (Decayed)

SL-16 DEB, 22620

SL-16 DEB, 42248 (Decayed)

SL-16 DEB, 39909 (Decayed)

SL-16 DEB, 39873

SL-16 DEB, 42236

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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.
8 mins	2026-09-13 00:55:35.382Z	349.637° N	2026-09-13 00:59:35.382Z	80.555° E	49.971°	2026-09-13 01:03:35.382Z	140.48° SSE
6 mins	2026-09-13 15:07:35.382Z	180.164° SSW	2026-09-13 15:09:35.382Z	139.187° SSE	53.279°	2026-09-13 15:13:35.382Z	33.574° NE

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-09-11T06:11:55.520Z)

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: 1 day ago