SL-16 DEB, 22357

Orbit data source: Space-Track

SL-16 DEB, 22357 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/22357?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/22357?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

22357, 1992-093AW

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 day ago

TLE from 1 day ago

0 SL-16 DEB
1 22357U 92093AW  25349.34094023  .00227613  00000-0  21283-2 0  9999
2 22357  70.8327 325.7845 0010200 185.4833 174.6258 15.66356948742691

Epoch: 2025-12-15T08:10Z

TLE epoch observation values (Epoch: 2025-12-15T08:10:57.235Z)

Latitude

0.00001°

Longitude

118.80513°

Altitude

378.749 km

Speed

7.679 km/s

True Right ascension

21h 43m 08s

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

18:32:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

374.016 km

Perigee altitude

360.255 km

Semi-major axis

6,745.273 km

Eccentricity

0.00102

Inclination

70.8327°

RAAN

325.7845°

Arg. of periapsis

185.4833°

True anomaly

174.63673°

Mean anomaly

174.6258°

Eccentric anomaly

174.63127°

Mean motion

3.91781 °/min

Orbital period

91.89 mins

BSTAR

0.0021283

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

SL-16 DEB, 22553 (Decayed)

SL-16 DEB, 22505 (Decayed)

SL-16 DEB, 22343

SL-16 DEB, 22367

SL-16 DEB, 22379

SL-16 DEB, 39867

SL-16 DEB, 39865

SL-16 DEB, 39847

SL-16 DEB, 39724

SL-16 DEB, 39722

SL-16 DEB, 23302

SL-16 DEB, 22403

SL-16 DEB, 39857

SL-16 DEB, 22394

SL-16 DEB, 22374

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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.
5 mins	2025-12-17 00:10:26.253Z	229.379° WSW	2025-12-17 00:12:26.253Z	275.432° WNW	30.047°	2025-12-17 00:15:26.253Z	5.504° 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, 22357 on other resources

View SL-16 DEB, 22357 on Heavens-Above

View SL-16 DEB, 22357 on Keep Track

View SL-16 DEB, 22357 on Celestrak

View SL-16 DEB, 22357 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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