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SL-12 R/B(2), 29673

Orbit data source: Space-Track

SL-12 R/B(2), 29673 is space debris in MEO originally from a launch on Mon, 25 Dec 2006 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/29673?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/29673?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29673, 2006-062D

Orbit

MEO

Last TLE update

5 hours ago

Origin

Khrunichev State Research and Production Space Center (CIS)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

BLOK DM2, 11D58M

Mass

2,440 kg wet, 2,440 kg dry

Launch date (UTC)

2006-12-25 (19 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 6.3 m

Radar Cross Section

23.684 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 5 hours ago

0 SL-12 R/B(2)
1 29673U 06062D   25183.46448337  .00000077  00000-0  00000+0 0  9992
2 29673  64.7026 205.2873 0027524 193.9583 348.7000  2.13404448144549

Epoch: 2025-07-02T11:08Z

TLE epoch observation values (Epoch: 2025-07-02T11:08:51.363Z)

Latitude

-2.35924°

Longitude

-61.5523°

Altitude

19,037.898 km

Speed

3.966 km/s

True Right ascension

01h 45m 37s

True Declination

-2° 21' 19"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-5.27353°

Longitude

114.82667°

Altitude

19,173.188 km

Speed

3.945 km/s

Apparent Right ascension

13h 56m 06s

Apparent Declination

-12° 20' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:13:37

Azimuth

57.348° ENE

Elevation

-49.067°

Doppler factor

1

Orbital elements

Apogee altitude

19,175.547 km

Perigee altitude

19,035.265 km

Semi-major axis

25,483.543 km

Eccentricity

0.00275

Inclination

64.7026°

RAAN

205.2873°

Arg. of periapsis

193.9583°

True anomaly

Unknown

Mean anomaly

348.7°

Eccentric anomaly

Unknown

Mean motion

0.53352 °/min

Orbital period

674.76 mins

BSTAR

0

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Other satellites on launch #62 in the year 2006 (2006-12-25 UTC)

COSMOS 2425 (GLONASS), 29670

COSMOS 2426 (GLONASS), 29671

COSMOS 2424 (GLONASS), 29672

SL-12 R/B(1), 29674 (Decayed)

SL-12 PLAT, 29675 (Decayed)

SL-12 R/B(AUX MOTOR), 29680

SL-12 R/B(AUX MOTOR), 29682

SL-12 DEB, 41768

SL-12 DEB, 41805

SL-12 DEB, 41806

SL-12 DEB, 41807

SL-12 DEB, 41808

SL-12 DEB, 41809 (Decayed)

SL-12 DEB, 41810

SL-12 R/B(2) Visibility forecast

Observer location: undefined°, undefined°

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.
359 mins	2025-07-03 03:15:14.231Z	210.663° SW	2025-07-03 05:48:14.231Z	313.815° NW	42.152°	2025-07-03 09:14:14.231Z	98.567° ESE

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Check out SL-12 R/B(2), 29673 on other resources

View SL-12 R/B(2), 29673 on Heavens-Above

View SL-12 R/B(2), 29673 on Keep Track

View SL-12 R/B(2), 29673 on Celestrak

View SL-12 R/B(2), 29673 on Gunter's Space Page

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

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