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: 7 hours ago

TLE from 7 hours ago
0 SL-3 R/B
1 14208U 83075B   26087.15701615  .00012445  00000-0  32339-3 0  9996
2 14208  97.6141  92.4397 0022179 158.7580 201.4591 15.38842463332996
Epoch: 2026-03-28T03:46Z
TLE epoch observation values (Epoch: 2026-03-28T03:46:06.195Z)
Latitude
0.00002°
Longitude
-149.66741°
Altitude
466.742 km
Speed
7.625 km/s
True Right ascension
06h 09m 45s
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
16:12:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.617 km
Perigee altitude
431.345 km
Semi-major axis
6,824.618 km
Eccentricity
0.00222
Inclination
97.6141°
RAAN
92.4397°
Arg. of periapsis
158.758°
True anomaly
201.36636°
Mean anomaly
201.4591°
Eccentric anomaly
201.41271°
Mean motion
3.84969 °/min
Orbital period
93.51 mins
BSTAR
0.00032339

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