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SL-12 R/B(2), 33471

Orbit data source: Space-Track

SL-12 R/B(2), 33471 is space debris in MEO 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/33471?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

33471, 2008-067F

Orbit

MEO

Country

CIS

Related business

Khrunichev State Research and Production Space Center (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

BLOK DM2, 11D58M

Mass

2,440 kg wet, 2,440 kg dry

Launch date (UTC)

2008-12-25 (17 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 3.5 m

Radar Cross Section

26.008 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago

0 SL-12 R/B(2)
1 33471U 08067F   26064.89223824 -.00000003  00000-0  00000-0 0  9999
2 33471  64.7567  72.5096 0005057 335.9857 204.5807  2.13248916133897

Epoch: 2026-03-05T21:24Z

TLE epoch observation values (Epoch: 2026-03-05T21:24:49.383Z)

Latitude

-0.51974°

Longitude

127.90385°

Altitude

19,130.511 km

Speed

3.952 km/s

True Right ascension

16h 50m 58s

True Declination

0° 31' 08"

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

14:03:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

19,130.687 km

Perigee altitude

19,104.9 km

Semi-major axis

25,495.931 km

Eccentricity

0.00051

Inclination

64.7567°

RAAN

72.5096°

Arg. of periapsis

335.9857°

True anomaly

204.55661°

Mean anomaly

204.5807°

Eccentric anomaly

204.56865°

Mean motion

0.53313 °/min

Orbital period

675.25 mins

BSTAR

0

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

SL-12 PLAT, 33470 (Decayed)

SL-12 DEB, 41560

SL-12 DEB, 41641

SL-12 DEB, 41562

COSMOS 2449 (GLONASS), 33467

SL-12 R/B(AUX MOTOR), 33473

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

COSMOS 2448 (GLONASS), 33468

SL-12 DEB, 41642

SL-12 R/B(1), 33469 (Decayed)

COSMOS 2447 (GLONASS), 33466

SL-12 DEB, 41649

SL-12 DEB, 41561 (Decayed)

SL-12 DEB, 41643

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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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.
318 mins	2026-03-07 00:40:35.860Z	189.824° SSW	2026-03-07 03:00:35.860Z	289.528° WNW	44.719°	2026-03-07 05:58:35.860Z	65.623° ENE

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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), 33471 on other resources

View SL-12 R/B(2), 33471 on Heavens-Above

View SL-12 R/B(2), 33471 on Keep Track

View SL-12 R/B(2), 33471 on Celestrak

View SL-12 R/B(2), 33471 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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