SL-16 DEB, 22453

Orbit data source: Space-Track

SL-16 DEB, 22453 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/22453?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22453, 1992-093ES

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 22453U 92093ES  25348.90645853  .00000664  00000-0  52488-3 0  9997
2 22453  70.8030 149.6212 0167922 349.6272 134.6162 13.88880563661546

Epoch: 2025-12-14T21:45Z

TLE epoch observation values (Epoch: 2025-12-14T21:45:18.016Z)

Latitude

50.2779°

Longitude

-105.1552°

Altitude

1,027.278 km

Speed

7.299 km/s

True Right ascension

20h 19m 55s

True Declination

50° 06' 54"

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

00:24:34

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,053.254 km

Perigee altitude

807.797 km

Semi-major axis

7,308.662 km

Eccentricity

0.01679

Inclination

70.803°

RAAN

149.6212°

Arg. of periapsis

349.6272°

True anomaly

135.96589°

Mean anomaly

134.6162°

Eccentric anomaly

135.29303°

Mean motion

3.47365 °/min

Orbital period

103.64 mins

BSTAR

0.00052488

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

SL-16 DEB, 22546 (Decayed)

SL-16 DEB, 39859 (Decayed)

SL-16 DEB, 22547 (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	2025-12-16 11:18:12.052Z	161.537° S	2025-12-16 11:22:12.052Z	103.177° ESE	29.365°	2025-12-16 11:27:12.052Z	41.562° NE
9 mins	2025-12-16 13:04:12.052Z	245.787° WSW	2025-12-16 13:08:12.052Z	303.676° NW	28.677°	2025-12-16 13:13:12.052Z	5.465° NNE
8 mins	2025-12-16 20:23:12.052Z	13.649° NNE	2025-12-16 20:26:12.052Z	48.775° ENE	22.496°	2025-12-16 20:31:12.052Z	102.121° ESE
11 mins	2025-12-16 22:08:12.052Z	327.509° NNW	2025-12-16 22:13:12.052Z	244.406° WSW	42.075°	2025-12-16 22:19:12.052Z	172.02° 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, 22453 on other resources

View SL-16 DEB, 22453 on Heavens-Above

View SL-16 DEB, 22453 on Keep Track

View SL-16 DEB, 22453 on Celestrak

View SL-16 DEB, 22453 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, 22453

Orbit data source: Space-Track

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

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-14T21:45:18.016Z)

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, 22453 on other resources

Documentation

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