SL-16 DEB, 22327

Orbit data source: Space-Track

SL-16 DEB, 22327 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/22327?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22327, 1992-093Q

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, 0.5 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 SL-16 DEB
1 22327U 92093Q   25298.09867854  .00012644  00000-0  10635-2 0  9996
2 22327  71.1145 190.5824 0059735   8.6580 101.0681 14.96983314728093

Epoch: 2025-10-25T02:22Z

TLE epoch observation values (Epoch: 2025-10-25T02:22:05.825Z)

Latitude

62.58915°

Longitude

-99.67663°

Altitude

594.646 km

Speed

7.564 km/s

True Right ascension

21h 58m 19s

True Declination

62° 26' 42"

Sunlit

Object was in full shadow 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

06:03:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

615.586 km

Perigee altitude

532.528 km

Semi-major axis

6,952.194 km

Eccentricity

0.00597

Inclination

71.1145°

RAAN

190.5824°

Arg. of periapsis

8.658°

True anomaly

101.7389°

Mean anomaly

101.0681°

Eccentric anomaly

101.4036°

Mean motion

3.74421 °/min

Orbital period

96.15 mins

BSTAR

0.0010635

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

SL-16 DEB, 22548 (Decayed)

SL-16 DEB, 22373 (Decayed)

SL-16 DEB, 22420 (Decayed)

SL-16 DEB, 22484 (Decayed)

SL-16 DEB, 22538 (Decayed)

SL-16 DEB, 22427 (Decayed)

SL-16 DEB, 22391 (Decayed)

SL-16 DEB, 22402 (Decayed)

SL-16 DEB, 22550 (Decayed)

SL-16 DEB, 22462 (Decayed)

SL-16 DEB, 22482 (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.
7 mins	2025-10-25 18:02:44.577Z	182.91° SSW	2025-10-25 18:05:44.577Z	122.819° SE	37.922°	2025-10-25 18:09:44.577Z	33.216° NE
7 mins	2025-10-26 04:05:44.577Z	335.965° NNW	2025-10-26 04:08:44.577Z	314.373° NW	44.606°	2025-10-26 04:12:44.577Z	160.049° S

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, 22327 on other resources

View SL-16 DEB, 22327 on Heavens-Above

View SL-16 DEB, 22327 on Keep Track

View SL-16 DEB, 22327 on Celestrak

View SL-16 DEB, 22327 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, 22327

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2025-10-25T02:22:05.825Z)

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, 22327 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago