SL-12 R/B(2), 22966

Orbit data source: Space-Track

SL-12 R/B(2), 22966 is space debris in GEO originally from a launch on Thu, 20 Jan 1994 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.

Not visible in the next 10 days

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Iframe URL

https://www.satcat.com/sats-embedded/22966?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22966, 1994-002D

Orbit

GEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

BLOK DM2, Unknown motor

Mass

2,560 kg wet, 2,560 kg dry

Launch date (UTC)

1994-01-20 (33 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 3.6 m

Radar Cross Section

23.597 m², Large (>1 m²)

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Last TLE update: 15 hours ago

TLE from 15 hours ago

0 SL-12 R/B(2)
1 22966U 94002D   26256.49803157 -.00000242  00000-0  00000-0 0  9997
2 22966  13.8824 343.4460 0040895 151.4044 201.5428  0.99473084117951

Epoch: 2026-09-13T11:57Z

TLE epoch observation values (Epoch: 2026-09-13T11:57:09.927Z)

Latitude

-1.73402°

Longitude

164.64188°

Altitude

36,173.723 km

Speed

3.055 km/s

True Right ascension

22h 25m 42s

True Declination

-1° 43' 56"

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

19:49:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

36,186.33 km

Perigee altitude

35,839.614 km

Semi-major axis

42,391.109 km

Eccentricity

0.00409

Inclination

13.8824°

RAAN

343.446°

Arg. of periapsis

151.4044°

True anomaly

201.37154°

Mean anomaly

201.5428°

Eccentric anomaly

201.45709°

Mean motion

0.24867 °/min

Orbital period

1,447.68 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #2 in the year 1994 (1994-01-20 UTC)

SL-12 R/B(AUX MOTOR), 22968 (Decayed)

SL-12 R/B(AUX MOTOR), 22967 (Decayed)

GALS 1, 22963

SL-12 PLAT, 22965 (Decayed)

SL-12 R/B(1), 22964 (Decayed)

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SL-12 R/B(2) Visibility

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22966 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), 22966 on other resources

View SL-12 R/B(2), 22966 on Heavens-Above

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View SL-12 R/B(2), 22966 on Celestrak

View SL-12 R/B(2), 22966 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), 22966

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-09-13T11:57:09.927Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #2 in the year 1994 (1994-01-20 UTC)

SL-12 R/B(2) Visibility

22966 neighbors

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 22966 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago