SL-12 R/B(2), 22213

Orbit data source: Space-Track

SL-12 R/B(2), 22213 is space debris in GEO originally from a launch on Fri, 30 Oct 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/22213?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22213, 1992-074D

Orbit

GEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

NPO Energiya

Mission

Spacecraft

Bus & Motor

BLOK DM, Unknown motor

Mass

2,440 kg wet, 2,440 kg dry

Launch date (UTC)

1992-10-30 (33 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 3.1 m

Radar Cross Section

23.597 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago

0 SL-12 R/B(2)
1 22213U 92074D   25349.53754068 -.00000220  00000-0  00000-0 0  9998
2 22213  13.3853 344.1588 0020086 150.4839  41.2162  1.01145515123919

Epoch: 2025-12-15T12:54Z

TLE epoch observation values (Epoch: 2025-12-15T12:54:03.514Z)

Latitude

-2.73551°

Longitude

-102.25474°

Altitude

35,480.48 km

Speed

3.088 km/s

True Right ascension

11h 42m 46s

True Declination

-2° 43' 58"

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

03:22:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,628.619 km

Perigee altitude

35,460.208 km

Semi-major axis

41,922.55 km

Eccentricity

0.00201

Inclination

13.3853°

RAAN

344.1588°

Arg. of periapsis

150.4839°

True anomaly

41.36815°

Mean anomaly

41.2162°

Eccentric anomaly

41.29214°

Mean motion

0.25286 °/min

Orbital period

1,423.74 mins

BSTAR

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Other satellites on launch #74 in the year 1992 (1992-10-30 UTC)

SL-12 R/B(1), 22211 (Decayed)

EKRAN 20, 22210

SL-12 PLAT, 22212 (Decayed)

SL-12 R/B(AUX MOTOR), 22216 (Decayed)

SL-12 R/B(AUX MOTOR), 22215 (Decayed)

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SL-12 R/B(2) 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.
1440 mins	2025-12-16 04:42:55.057Z	170.707° S	2025-12-16 05:51:55.057Z	169.168° S	40.475°	2025-12-17 04:42:55.057Z	163.885° S

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22213 neighbors

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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-12 R/B(2), 22213 on other resources

View SL-12 R/B(2), 22213 on Heavens-Above

View SL-12 R/B(2), 22213 on Keep Track

View SL-12 R/B(2), 22213 on Celestrak

View SL-12 R/B(2), 22213 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-12 R/B(2), 22213

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2025-12-15T12:54:03.514Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #74 in the year 1992 (1992-10-30 UTC)

SL-12 R/B(2) Visibility forecast

22213 neighbors

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 22213 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago