SL-12 R/B(2), 23270

Orbit data source: Space-Track

SL-12 R/B(2), 23270 is space debris in GEO originally from a launch on Wed, 21 Sep 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.

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https://www.satcat.com/sats-embedded/23270?theme=dark&initialShowStats=false

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Identifier

23270, 1994-060D

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)

1994-09-21 (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: 18 hours ago

TLE from 18 hours ago

0 SL-12 R/B(2)
1 23270U 94060D   26061.60509742  .00000092  00000-0  00000+0 0  9991
2 23270  14.2900 350.8863 0006146 152.8431  84.4224  1.00072411114473

Epoch: 2026-03-02T14:31Z

TLE epoch observation values (Epoch: 2026-03-02T14:31:20.417Z)

Latitude

-11.99699°

Longitude

-150.80202°

Altitude

35,842.013 km

Speed

3.073 km/s

True Right ascension

15h 09m 42s

True Declination

-11° 59' 07"

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

11:59:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,869.503 km

Perigee altitude

35,817.604 km

Semi-major axis

42,221.69 km

Eccentricity

0.00061

Inclination

14.29°

RAAN

350.8863°

Arg. of periapsis

152.8431°

True anomaly

84.4925°

Mean anomaly

84.4224°

Eccentric anomaly

84.45745°

Mean motion

0.25017 °/min

Orbital period

1,439.01 mins

BSTAR

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Other satellites on launch #60 in the year 1994 (1994-09-21 UTC)

SL-12 R/B(1), 23268 (Decayed)

COSMOS 2291, 23267

SL-12 PLAT, 23269 (Decayed)

SL-12 R/B(AUX MOTOR), 23272 (Decayed)

SL-12 R/B(AUX MOTOR), 23271 (Decayed)

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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	2026-03-03 08:15:22.817Z	243.997° WSW	2026-03-04 05:11:22.817Z	250.608° W	30.038°	2026-03-04 08:15:22.817Z	244.605° WSW

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23270 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), 23270 on other resources

View SL-12 R/B(2), 23270 on Heavens-Above

View SL-12 R/B(2), 23270 on Keep Track

View SL-12 R/B(2), 23270 on Celestrak

View SL-12 R/B(2), 23270 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), 23270

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: 2026-03-02T14:31:20.417Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #60 in the year 1994 (1994-09-21 UTC)

SL-12 R/B(2) Visibility forecast

23270 neighbors

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 23270 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 18 hours ago