SL-16 DEB, 39888

Orbit data source: Space-Track

SL-16 DEB, 39888 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/39888?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39888, 1993-016BN

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, 1.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago

0 SL-16 DEB
1 39888U 93016BN  26071.27219495  .00008633  00000-0  24137-2 0  9999
2 39888  70.9494 288.2031 0074891 161.0089 199.3869 14.44741918609787

Epoch: 2026-03-12T06:31Z

TLE epoch observation values (Epoch: 2026-03-12T06:31:57.643Z)

Latitude

-0.0001°

Longitude

20.28842°

Altitude

795.662 km

Speed

7.43 km/s

True Right ascension

19h 12m 48s

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

20:06:11

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

794.089 km

Perigee altitude

687.46 km

Semi-major axis

7,118.912 km

Eccentricity

0.00749

Inclination

70.9494°

RAAN

288.2031°

Arg. of periapsis

161.0089°

True anomaly

199.10452°

Mean anomaly

199.3869°

Eccentric anomaly

199.24546°

Mean motion

3.61346 °/min

Orbital period

99.63 mins

BSTAR

0.0024137

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

SL-16 DEB, 42253 (Decayed)

SL-16 DEB *, 29096 (Decayed)

SL-16 DEB, 39897 (Decayed)

SL-16 DEB, 39900 (Decayed)

SL-16 DEB, 22576

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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	2026-03-25 22:25:19.992Z	349.034° N	2026-03-25 22:29:19.992Z	76.2° E	38.892°	2026-03-25 22:33:19.992Z	140.372° SSE
8 mins	2026-03-26 12:57:19.992Z	204.33° SW	2026-03-26 13:01:19.992Z	7.148° NNE	43.866°	2026-03-26 13:05:19.992Z	21.932° NNE

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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, 39888 on other resources

View SL-16 DEB, 39888 on Heavens-Above

View SL-16 DEB, 39888 on Keep Track

View SL-16 DEB, 39888 on Celestrak

View SL-16 DEB, 39888 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, 39888

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 weeks ago

TLE from 2 weeks ago

TLE epoch observation values (Epoch: 2026-03-12T06:31:57.643Z)

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, 39888 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 weeks ago