SL-12 R/B(2), 23656

Orbit data source: Space-Track

SL-12 R/B(2), 23656 is space debris in GEO originally from a launch on Wed, 30 Aug 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.

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https://www.satcat.com/sats-embedded/23656?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

23656, 1995-045D

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)

1995-08-30 (31 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: 2 days ago

TLE from 2 days ago

0 SL-12 R/B(2)
1 23656U 95045D   26069.41772848  .00000089  00000-0  00000-0 0  9996
2 23656  14.4259 353.7790 0018354  50.9528 134.1287  1.00141783111670

Epoch: 2026-03-10T10:01Z

TLE epoch observation values (Epoch: 2026-03-10T10:01:31.740Z)

Latitude

-1.30441°

Longitude

-139.6115°

Altitude

35,876.98 km

Speed

3.069 km/s

True Right ascension

11h 55m 28s

True Declination

-1° 18' 11"

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

11:53:02

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,901.509 km

Perigee altitude

35,746.593 km

Semi-major axis

42,202.188 km

Eccentricity

0.00184

Inclination

14.4259°

RAAN

353.779°

Arg. of periapsis

50.9528°

True anomaly

134.27942°

Mean anomaly

134.1287°

Eccentric anomaly

134.20409°

Mean motion

0.25035 °/min

Orbital period

1,438.01 mins

BSTAR

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Other satellites on launch #45 in the year 1995 (1995-08-30 UTC)

SL-12 R/B(AUX MOTOR), 23661 (Decayed)

SL-12 R/B(1), 23654 (Decayed)

SL-12 PLAT, 23655 (Decayed)

SL-12 DEB, 23664 (Decayed)

SL-12 R/B(AUX MOTOR), 23660 (Decayed)

SL-12 DEB, 23663 (Decayed)

COSMOS 2319, 23653

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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	2026-03-12 07:33:39.091Z	232.629° WSW	2026-03-13 04:03:39.091Z	240.531° WSW	34.574°	2026-03-13 07:33:39.091Z	233.058° WSW

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23656 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), 23656 on other resources

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View SL-12 R/B(2), 23656 on Keep Track

View SL-12 R/B(2), 23656 on Celestrak

View SL-12 R/B(2), 23656 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), 23656

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-03-10T10:01:31.740Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #45 in the year 1995 (1995-08-30 UTC)

SL-12 R/B(2) Visibility forecast

23656 neighbors

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 23656 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago