SL-12 R/B(AUX MOTOR), 36406

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 36406 is space debris in HEO originally from a launch on Mon, 01 Mar 2010 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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<iframe src="https://www.satcat.com/sats-embedded/36406?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/36406?theme=dark&initialShowStats=false

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Identifier

36406, 2010-007G

Orbit

HEO

Country

CIS

Related business

Russian Space Forces (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

SOZ, Unknown motor

Mass

56 kg wet, 56 kg dry

Launch date (UTC)

2010-03-01 (16 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 0.6 m

Radar Cross Section

0.660 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago

0 SL-12 R/B(AUX MOTOR)
1 36406U 10007G   26151.35000047  .00000048  00000-0  28408-3 0  9998
2 36406  64.6295 218.7380 5658931 327.6385   7.7993  4.23094322182514

Epoch: 2026-05-31T08:24Z

TLE epoch observation values (Epoch: 2026-05-31T08:24:00.040Z)

Latitude

0.0001°

Longitude

-156.12151°

Altitude

1,054.921 km

Speed

9.088 km/s

True Right ascension

14h 34m 55s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

05:23:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

18,905.722 km

Perigee altitude

631.216 km

Semi-major axis

16,146.606 km

Eccentricity

0.56589

Inclination

64.6295°

RAAN

218.738°

Arg. of periapsis

327.6385°

True anomaly

32.78091°

Mean anomaly

7.7993°

Eccentric anomaly

17.60679°

Mean motion

1.05784 °/min

Orbital period

340.32 mins

BSTAR

0.00028408

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Other satellites on launch #7 in the year 2010 (2010-03-01 UTC)

SL-12 DEB, 36409 (Decayed)

SL-12 PLAT, 36405 (Decayed)

SL-12 DEB, 41700

SL-12 DEB, 48540

SL-12 DEB, 43685 (Decayed)

SL-12 DEB, 43580

SL-12 DEB, 43542

SL-12 DEB, 48541

COSMOS 2459 (GLONASS), 36400

SL-12 DEB, 36410 (Decayed)

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SL-12 R/B(AUX MOTOR) 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.
79 mins	2026-06-06 19:22:41.098Z	302.448° NW	2026-06-06 19:22:41.098Z	302.448° NW	21.493°	2026-06-06 20:41:41.098Z	277.388° WNW
61 mins	2026-06-07 04:59:41.098Z	179.936° S	2026-06-07 05:06:41.098Z	110.734° ESE	42.312°	2026-06-07 06:00:41.098Z	34.248° NE
247 mins	2026-06-07 10:55:41.098Z	306.651° NW	2026-06-07 12:08:41.098Z	50.933° ENE	40.776°	2026-06-07 15:02:41.098Z	149.942° SSE
139 mins	2026-06-07 17:03:41.098Z	328.641° NNW	2026-06-07 18:11:41.098Z	293.508° NW	31.418°	2026-06-07 19:22:41.098Z	265.934° W

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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(AUX MOTOR), 36406 on other resources

View SL-12 R/B(AUX MOTOR), 36406 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 36406 on Keep Track

View SL-12 R/B(AUX MOTOR), 36406 on Celestrak

View SL-12 R/B(AUX MOTOR), 36406 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(AUX MOTOR), 36406

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 days ago

TLE from 6 days ago

TLE epoch observation values (Epoch: 2026-05-31T08:24:00.040Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #7 in the year 2010 (2010-03-01 UTC)

SL-12 R/B(AUX MOTOR) Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(AUX MOTOR), 36406 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 days ago