SL-12 R/B(AUX MOTOR), 33472

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 33472 is space debris in HEO originally from a launch on Thu, 25 Dec 2008 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/33472?theme=dark&initialShowStats=false

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Identifier

33472, 2008-067G

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)

2008-12-25 (18 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: 2 days ago

TLE from 2 days ago

0 SL-12 R/B(AUX MOTOR)
1 33472U 08067G   26243.48864441 -.00000000  00000-0  10299-3 0  9991
2 33472  65.0407  33.1904 5578496 275.1204  26.8531  4.40026414275170

Epoch: 2026-08-31T11:43Z

TLE epoch observation values (Epoch: 2026-08-31T11:43:38.877Z)

Latitude

-0.00006°

Longitude

-122.4112°

Altitude

3,949.693 km

Speed

7.202 km/s

True Right ascension

02h 12m 40s

True Declination

0° 00' 00"

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

20:33:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

18,126.239 km

Perigee altitude

576.719 km

Semi-major axis

15,729.616 km

Eccentricity

0.55785

Inclination

65.0407°

RAAN

33.1904°

Arg. of periapsis

275.1204°

True anomaly

85.025°

Mean anomaly

26.8531°

Eccentric anomaly

52.06065°

Mean motion

1.10019 °/min

Orbital period

327.22 mins

BSTAR

0.00010299

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Other satellites on launch #67 in the year 2008 (2008-12-25 UTC)

SL-12 DEB, 44594 (Decayed)

SL-12 PLAT, 33470 (Decayed)

SL-12 DEB, 41650

SL-12 DEB, 41645

SL-12 DEB, 41644 (Decayed)

SL-12 DEB, 41561 (Decayed)

COSMOS 2447 (GLONASS), 33466

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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.
135 mins	2026-09-02 07:32:35.765Z	101.87° ESE	2026-09-02 08:14:35.765Z	55.221° ENE	24.337°	2026-09-02 09:47:35.765Z	25.68° NE
243 mins	2026-09-02 12:54:35.765Z	233.59° WSW	2026-09-02 13:41:35.765Z	314.134° NW	42.751°	2026-09-02 16:57:35.765Z	81.009° E
212 mins	2026-09-02 19:19:35.765Z	317.947° NNW	2026-09-02 22:06:35.765Z	271.973° WNW	42.96°	2026-09-02 22:51:35.765Z	188.575° SSW

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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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Check out SL-12 R/B(AUX MOTOR), 33472 on other resources

View SL-12 R/B(AUX MOTOR), 33472 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 33472 on Keep Track

View SL-12 R/B(AUX MOTOR), 33472 on Celestrak

View SL-12 R/B(AUX MOTOR), 33472 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), 33472

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: 2026-08-31T11:43:38.877Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #67 in the year 2008 (2008-12-25 UTC)

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

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(AUX MOTOR), 33472 on other resources

Documentation

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