SL-12 R/B(2), 23683

Orbit data source: Space-Track

SL-12 R/B(2), 23683 is space debris in GEO originally from a launch on Wed, 11 Oct 1995 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/23683?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

23683, 1995-054D

Orbit

GEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

BLOK DM, Unknown motor

Mass

2,440 kg wet, 2,440 kg dry

Launch date (UTC)

1995-10-11 (30 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)

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Last TLE update: 1 month ago

TLE from 1 month ago

0 SL-12 R/B(2)
1 23683U 95054D   25266.55764235 -.00000334  00000-0  00000+0 0  9993
2 23683  14.9636   1.1750 0018657 102.1833 233.8401  1.00279520109694

Epoch: 2025-09-23T13:23Z

TLE epoch observation values (Epoch: 2025-09-23T13:23:00.299Z)

Latitude

-6.06827°

Longitude

134.34171°

Altitude

35,831.443 km

Speed

3.071 km/s

True Right ascension

22h 30m 57s

True Declination

-6° 03' 44"

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

10:58:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,864.057 km

Perigee altitude

35,706.728 km

Semi-major axis

42,163.53 km

Eccentricity

0.00187

Inclination

14.9636°

RAAN

1.175°

Arg. of periapsis

102.1833°

True anomaly

233.66773°

Mean anomaly

233.8401°

Eccentric anomaly

233.75389°

Mean motion

0.25069 °/min

Orbital period

1,436.03 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #54 in the year 1995 (1995-10-11 UTC)

SL-12 PLAT, 23682 (Decayed)

SL-12 R/B(AUX MOTOR), 23684 (Decayed)

LUCH 1, 23680

SL-12 R/B(1), 23681 (Decayed)

SL-12 R/B(AUX MOTOR), 23685 (Decayed)

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SL-12 R/B(2) Visibility

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23683 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), 23683 on other resources

View SL-12 R/B(2), 23683 on Heavens-Above

View SL-12 R/B(2), 23683 on Keep Track

View SL-12 R/B(2), 23683 on Celestrak

View SL-12 R/B(2), 23683 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), 23683

Orbit data source: Space-Track

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

TLE from 1 month ago

TLE epoch observation values (Epoch: 2025-09-23T13:23:00.299Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #54 in the year 1995 (1995-10-11 UTC)

SL-12 R/B(2) Visibility

23683 neighbors

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 23683 on other resources

Documentation

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