SL-12 R/B(2), 22061

Orbit data source: Space-Track

SL-12 R/B(2), 22061 is space debris in MEO originally from a launch on Thu, 30 Jul 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/22061?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22061, 1992-047F

Orbit

MEO

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)

1992-07-30 (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: 3 days ago

TLE from 3 days ago

0 SL-12 R/B(2)
1 22061U 92047F   25346.40064661 -.00000061  00000-0  00000-0 0  9998
2 22061  64.2485 307.7173 0003009 279.6814 258.8782  2.13332134259917

Epoch: 2025-12-12T09:36Z

TLE epoch observation values (Epoch: 2025-12-12T09:36:55.867Z)

Latitude

1.27118°

Longitude

-98.48366°

Altitude

19,113.41 km

Speed

3.954 km/s

True Right ascension

08h 28m 22s

True Declination

1° 16' 09"

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

13:18:50

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

19,118.85 km

Perigee altitude

19,103.511 km

Semi-major axis

25,489.317 km

Eccentricity

0.0003

Inclination

64.2485°

RAAN

307.7173°

Arg. of periapsis

279.6814°

True anomaly

258.84437°

Mean anomaly

258.8782°

Eccentric anomaly

258.86128°

Mean motion

0.53334 °/min

Orbital period

674.99 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #47 in the year 1992 (1992-07-30 UTC)

SL-12 DEB, 28585 (Decayed)

SL-12 DEB, 28582

SL-12 DEB, 23616

SL-12 R/B(AUX MOTOR), 22066

SL-12 DEB, 28579 (Decayed)

SL-12 DEB, 34183

COSMOS 2205 (GLONASS), 22058

COSMOS 2206 (GLONASS), 22056

SL-12 DEB, 28586 (Decayed)

SL-12 DEB, 28588 (Decayed)

SL-12 DEB, 27805

SL-12 DEB, 28678 (Decayed)

SL-12 DEB, 28589 (Decayed)

SL-12 DEB, 38548 (Decayed)

SL-12 DEB, 28584

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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.
305 mins	2025-12-15 21:08:17.329Z	182.506° SSW	2025-12-15 23:27:17.329Z	281.815° WNW	45°	2025-12-16 02:13:17.329Z	56.775° ENE
115 mins	2025-12-16 12:12:17.329Z	334.783° NNW	2025-12-16 13:08:17.329Z	308.957° NW	18.152°	2025-12-16 14:07:17.329Z	279.72° WNW

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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), 22061 on other resources

View SL-12 R/B(2), 22061 on Heavens-Above

View SL-12 R/B(2), 22061 on Keep Track

View SL-12 R/B(2), 22061 on Celestrak

View SL-12 R/B(2), 22061 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), 22061

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-12-12T09:36:55.867Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #47 in the year 1992 (1992-07-30 UTC)

SL-12 R/B(2) Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 22061 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago