SL-16 DEB, 39709

Orbit data source: Space-Track

SL-16 DEB, 39709 is space debris in LEO originally from a launch on Fri, 25 Dec 1992 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/39709?theme=dark&initialShowStats=false

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Identifier

39709, 1992-093JZ

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1992-12-25 (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: 22 hours ago

TLE from 22 hours ago

0 SL-16 DEB
1 39709U 92093JZ  26133.00305112  .00000380  00000-0  29105-3 0  9999
2 39709  71.1475  13.1828 0141322  97.5256 264.1937 13.94625161613308

Epoch: 2026-05-13T00:04Z

TLE epoch observation values (Epoch: 2026-05-13T00:04:23.616Z)

Latitude

-0.00002°

Longitude

141.31507°

Altitude

926.718 km

Speed

7.383 km/s

True Right ascension

00h 52m 43s

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

06:52:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,013.4 km

Perigee altitude

807.394 km

Semi-major axis

7,288.534 km

Eccentricity

0.01413

Inclination

71.1475°

RAAN

13.1828°

Arg. of periapsis

97.5256°

True anomaly

262.58566°

Mean anomaly

264.1937°

Eccentric anomaly

263.38937°

Mean motion

3.48805 °/min

Orbital period

103.21 mins

BSTAR

0.00029105

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Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB, 22414 (Decayed)

SL-16 DEB, 22329 (Decayed)

SL-16 DEB, 22545

SL-16 DEB, 22334 (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.
9 mins	2026-05-14 02:26:51.829Z	353.058° N	2026-05-14 02:30:51.829Z	47.074° ENE	33.838°	2026-05-14 02:35:51.829Z	129.551° SE
7 mins	2026-05-14 04:13:51.829Z	296.905° NW	2026-05-14 04:16:51.829Z	253.736° W	22.291°	2026-05-14 04:20:51.829Z	207.04° SW
5 mins	2026-05-14 15:48:51.829Z	122.449° SE	2026-05-14 15:50:51.829Z	98.108° ESE	16.172°	2026-05-14 15:53:51.829Z	64.019° ENE
9 mins	2026-05-14 17:31:51.829Z	218.888° SW	2026-05-14 17:35:51.829Z	300.679° NW	41.504°	2026-05-14 17:40:51.829Z	15.578° 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, 39709 on other resources

View SL-16 DEB, 39709 on Heavens-Above

View SL-16 DEB, 39709 on Keep Track

View SL-16 DEB, 39709 on Celestrak

View SL-16 DEB, 39709 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, 39709

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 22 hours ago

TLE from 22 hours ago

TLE epoch observation values (Epoch: 2026-05-13T00:04:23.616Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 DEB, 39709 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 22 hours ago