SL-6 R/B(2), 23587

Orbit data source: Space-Track

SL-6 R/B(2), 23587 is space debris in HEO originally from a launch on Wed, 24 May 1995 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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
23587, 1995-026D
Orbit
HEO
Country
Flag of CISCIS
Related business
Manufacturer
RKKE
Mission
Spacecraft
Bus & Motor
BLOK-L, Unknown motor
Mass
900 kg wet, 900 kg dry
Launch date (UTC)
1995-05-24 (31 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.6 m
Radar Cross Section
8.039 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 SL-6 R/B(2)
1 23587U 95026D   26152.34279234  .00000940  00000-0  00000-0 0  9990
2 23587  66.6414 206.3937 6518558  31.6908 354.8797  2.03313040230261
Epoch: 2026-06-01T08:13Z
TLE epoch observation values (Epoch: 2026-06-01T08:13:37.258Z)
Latitude
-0.00006°
Longitude
-166.84266°
Altitude
3,335.56 km
Speed
8.181 km/s
True Right ascension
13h 45m 34s
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
22:33:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,097.641 km
Perigee altitude
2,784.793 km
Semi-major axis
26,319.354 km
Eccentricity
0.65186
Inclination
66.6414°
RAAN
206.3937°
Arg. of periapsis
31.6908°
True anomaly
329.18121°
Mean anomaly
354.8797°
Eccentric anomaly
345.5769°
Mean motion
0.50831 °/min
Orbital period
708.23 mins
BSTAR
0
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Other satellites on launch #26 in the year 1995 (1995-05-24 UTC)

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