SL-23 R/B, 32782

Orbit data source: Space-Track

SL-23 R/B, 32782 is space debris originally from a launch on Sun, 27 Apr 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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Identifier
32782, 2008-020B
Orbit
Active
Country
Flag of CISCIS
Related business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,000 kg wet, 1,000 kg dry
Launch date (UTC)
2008-04-27 (18 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.7 m
Radar Cross Section
8.880 m², Large (>1 m²)

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

TLE from 2 days ago
0 SL-23 R/B
1 32782U 08020B   26171.23586490 -.00000088  00000-0  00000+0 0  9992
2 32782  59.0278  31.4820 0034384 260.5927 276.8729  1.67952033111309
Epoch: 2026-06-20T05:39Z
TLE epoch observation values (Epoch: 2026-06-20T05:39:38.727Z)
Latitude
2.51534°
Longitude
-143.37535°
Altitude
23,505.805 km
Speed
3.653 km/s
True Right ascension
13h 59m 57s
True Declination
2° 30' 42"
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
23:08:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,620.426 km
Perigee altitude
23,414.839 km
Semi-major axis
29,895.769 km
Eccentricity
0.00344
Inclination
59.0278°
RAAN
31.482°
Arg. of periapsis
260.5927°
True anomaly
276.48152°
Mean anomaly
276.8729°
Eccentric anomaly
276.67723°
Mean motion
0.41988 °/min
Orbital period
857.38 mins
BSTAR
0
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Other satellites on launch #20 in the year 2008 (2008-04-27 UTC)

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