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

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 29680 is space debris in HEO 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 URL

https://www.satcat.com/sats-embedded/29680?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29680, 2006-062G

Orbit

HEO

Last TLE update

2 days ago

Origin

Russian Strategic Rocket Forces (CIS)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

SOZ, Unknown motor

Mass

56 kg wet, 56 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, 1.1 m

Radar Cross Section

0.660 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 days ago

0 SL-12 R/B(AUX MOTOR)
1 29680U 06062G   25181.39178824  .00000034  00000-0 -31375-4 0  9999
2 29680  65.1595 161.9356 5670008 228.2014  67.2476  4.25850916185459

Epoch: 2025-06-30T09:24Z

TLE epoch observation values (Epoch: 2025-06-30T09:24:10.503Z)

Latitude

-0°

Longitude

102.17913°

Altitude

11,177.409 km

Speed

4.541 km/s

True Right ascension

10h 47m 42s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

58.35597°

Longitude

150.01328°

Altitude

16,698.49 km

Speed

3.126 km/s

Apparent Right ascension

14h 08m 57s

Apparent Declination

42° 29' 44"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

02:33:32

Azimuth

4.565° NNE

Elevation

-7.401°

Doppler factor

Orbital elements

Apogee altitude

18,814.2 km

Perigee altitude

583.099 km

Semi-major axis

16,076.786 km

Eccentricity

0.567

Inclination

65.1595°

RAAN

161.9356°

Arg. of periapsis

228.2014°

True anomaly

Unknown

Mean anomaly

67.2476°

Eccentric anomaly

Unknown

Mean motion

1.06474 °/min

Orbital period

338.11 mins

BSTAR

-0.000031375

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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(2), 29673

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

SL-12 PLAT, 29675 (Decayed)

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

SL-12 DEB, 41809 (Decayed)

SL-12 DEB, 41810

SL-12 R/B(AUX MOTOR) 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.
136 mins	2025-07-02 18:43:25.378Z	75.152° E	2025-07-02 20:00:25.378Z	50.164° ENE	20.508°	2025-07-02 20:59:25.378Z	27.755° NE
251 mins	2025-07-02 23:07:25.378Z	189.848° SSW	2025-07-03 01:03:25.378Z	279.099° WNW	44.726°	2025-07-03 03:18:25.378Z	47.716° ENE
149 mins	2025-07-03 06:52:25.378Z	307.292° NW	2025-07-03 09:07:25.378Z	64.824° ENE	44.796°	2025-07-03 09:21:25.378Z	144.743° SSE

Authenticating...

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Check out SL-12 R/B(AUX MOTOR), 29680 on other resources

View SL-12 R/B(AUX MOTOR), 29680 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 29680 on Keep Track

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

View SL-12 R/B(AUX MOTOR), 29680 on Gunter's Space Page

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