SL-3 R/B, 14208

Orbit data source: Space-Track

SL-3 R/B, 14208 is space debris in SSO originally from a launch on Sun, 24 Jul 1983 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
14208, 1983-075B
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
Progress
Mission
Spacecraft
Bus & Motor
BLOK-E, Unknown motor
Mass
1,440 kg wet, 1,440 kg dry
Launch date (UTC)
1983-07-24 (43 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

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

TLE from 2 days ago
0 SL-3 R/B
1 14208U 83075B   26171.44668627  .00007944  00000-0  19656-3 0  9992
2 14208  97.6107 180.0842 0019624 216.5803 143.4104 15.40541433345961
Epoch: 2026-06-20T10:43Z
TLE epoch observation values (Epoch: 2026-06-20T10:43:13.693Z)
Latitude
-0.00001°
Longitude
110.61596°
Altitude
458.384 km
Speed
7.632 km/s
True Right ascension
12h 00m 20s
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
00:51:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.84 km
Perigee altitude
428.075 km
Semi-major axis
6,819.595 km
Eccentricity
0.00196
Inclination
97.6107°
RAAN
180.0842°
Arg. of periapsis
216.5803°
True anomaly
143.54418°
Mean anomaly
143.4104°
Eccentric anomaly
143.47732°
Mean motion
3.85394 °/min
Orbital period
93.41 mins
BSTAR
0.00019656

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