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 (32 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 3.1 m

Radar Cross Section

23.597 m², Large (>1 m²)

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Last TLE update: 18 hours ago

TLE from 18 hours ago

0 SL-12 R/B(2)
1 22966U 94002D   25258.57096648 -.00000350  00000-0  00000-0 0  9996
2 22966  14.1038 346.0753 0042557 143.2200 206.8700  0.99471283114346

Epoch: 2025-09-15T13:42Z

TLE epoch observation values (Epoch: 2025-09-15T13:42:11.503Z)

Latitude

-2.46429°

Longitude

135.91589°

Altitude

36,174.031 km

Speed

3.055 km/s

True Right ascension

22h 24m 57s

True Declination

-2° 27' 43"

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

00:31:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

36,193.887 km

Perigee altitude

35,833.075 km

Semi-major axis

42,391.618 km

Eccentricity

0.00426

Inclination

14.1038°

RAAN

346.0753°

Arg. of periapsis

143.22°

True anomaly

206.65063°

Mean anomaly

206.87°

Eccentric anomaly

206.76021°

Mean motion

0.24867 °/min

Orbital period

1,447.7 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)

GALS 1, 22963

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

SL-12 PLAT, 22965 (Decayed)

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

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

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

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: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2025-09-15T13:42:11.503Z)

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: 18 hours ago