SL-16 DEB, 39300

Orbit data source: Space-Track

SL-16 DEB, 39300 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 src="https://www.satcat.com/sats-embedded/39300?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/39300?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39300, 1992-093JR

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: 1 week ago

TLE from 1 week ago

0 SL-16 DEB
1 39300U 92093JR  26034.13117040  .00000210  00000-0  17428-3 0  9998
2 39300  71.1232 322.9452 0102153 133.0585 227.9139 13.96902208631213

Epoch: 2026-02-03T03:08Z

TLE epoch observation values (Epoch: 2026-02-03T03:08:53.122Z)

Latitude

-0.00006°

Longitude

142.40733°

Altitude

957.215 km

Speed

7.348 km/s

True Right ascension

21h 31m 46s

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

09:15:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

976.846 km

Perigee altitude

828.099 km

Semi-major axis

7,280.609 km

Eccentricity

0.01022

Inclination

71.1232°

RAAN

322.9452°

Arg. of periapsis

133.0585°

True anomaly

227.05257°

Mean anomaly

227.9139°

Eccentric anomaly

227.4825°

Mean motion

3.49375 °/min

Orbital period

103.04 mins

BSTAR

0.00017428

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

SL-16 DEB, 26979 (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.
8 mins	2026-02-12 17:33:28.637Z	148.113° SSE	2026-02-12 17:37:28.637Z	101.904° ESE	21.495°	2026-02-12 17:41:28.637Z	54.319° ENE
9 mins	2026-02-12 19:18:28.637Z	228.993° WSW	2026-02-12 19:22:28.637Z	294.839° NW	37.188°	2026-02-12 19:27:28.637Z	10.357° NNE
9 mins	2026-02-13 04:19:28.637Z	340.783° N	2026-02-13 04:23:28.637Z	21.185° NNE	43.844°	2026-02-13 04:28:28.637Z	152.698° 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, 39300 on other resources

View SL-16 DEB, 39300 on Heavens-Above

View SL-16 DEB, 39300 on Keep Track

View SL-16 DEB, 39300 on Celestrak

View SL-16 DEB, 39300 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, 39300

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 week ago

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-02-03T03:08:53.122Z)

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, 39300 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 week ago