SL-16 DEB, 39305

Orbit data source: Space-Track

SL-16 DEB, 39305 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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https://www.satcat.com/sats-embedded/39305?theme=dark&initialShowStats=false

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Identifier

39305, 1992-093JW

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: 3 weeks ago

TLE from 3 weeks ago

0 SL-16 DEB
1 39305U 92093JW  26111.72980847  .00000086  00000-0  82684-4 0  9995
2 39305  70.9587 116.9059 0089169  90.7125 270.4209 14.02404719249322

Epoch: 2026-04-21T17:30Z

TLE epoch observation values (Epoch: 2026-04-21T17:30:55.451Z)

Latitude

-0.00002°

Longitude

4.37344°

Altitude

887.965 km

Speed

7.408 km/s

True Right ascension

07h 47m 37s

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

18:39:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

948.172 km

Perigee altitude

818.67 km

Semi-major axis

7,261.558 km

Eccentricity

0.00892

Inclination

70.9587°

RAAN

116.9059°

Arg. of periapsis

90.7125°

True anomaly

269.3991°

Mean anomaly

270.4209°

Eccentric anomaly

269.91°

Mean motion

3.50751 °/min

Orbital period

102.64 mins

BSTAR

0.000082684

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

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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	2026-05-13 20:18:11.267Z	152.801° SSE	2026-05-13 20:22:11.267Z	101.831° ESE	23.045°	2026-05-13 20:26:11.267Z	51.289° ENE
8 mins	2026-05-13 22:03:11.267Z	236.884° WSW	2026-05-13 22:07:11.267Z	308.283° NW	33.225°	2026-05-13 22:11:11.267Z	5.67° NNE
4 mins	2026-05-14 05:19:11.267Z	36.287° NE	2026-05-14 05:20:11.267Z	47.964° ENE	14.061°	2026-05-14 05:23:11.267Z	80.132° E
9 mins	2026-05-14 07:02:11.267Z	337.604° N	2026-05-14 07:06:11.267Z	140.262° SSE	44.914°	2026-05-14 07:11:11.267Z	157.855° 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, 39305 on other resources

View SL-16 DEB, 39305 on Heavens-Above

View SL-16 DEB, 39305 on Keep Track

View SL-16 DEB, 39305 on Celestrak

View SL-16 DEB, 39305 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, 39305

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 weeks ago

TLE from 3 weeks ago

TLE epoch observation values (Epoch: 2026-04-21T17:30:55.451Z)

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, 39305 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 weeks ago