SL-8 R/B, 1575

Orbit data source: Space-Track

SL-8 R/B, 1575 is space debris in LEO originally from a launch on Fri, 03 Sep 1965 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
1575, 1965-070F
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
S3, Unknown motor
Mass
1,434 kg wet, 1,434 kg dry
Launch date (UTC)
1965-09-03 (60 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: 12 hours ago

TLE from 12 hours ago
0 SL-8 R/B
1 01575U 65070F   25353.69536424 -.00000063  00000-0  19836-3 0  9993
2 01575  56.1235 241.5843 0098451 197.1300 178.5948 12.57012800768196
Epoch: 2025-12-19T16:41Z
TLE epoch observation values (Epoch: 2025-12-19T16:41:19.470Z)
Latitude
13.02154°
Longitude
-88.39134°
Altitude
1,512.526 km
Speed
7.075 km/s
True Right ascension
16h 41m 53s
True Declination
12° 57' 12"
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
03:17:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,512.034 km
Perigee altitude
1,358.19 km
Semi-major axis
7,813.249 km
Eccentricity
0.00985
Inclination
56.1235°
RAAN
241.5843°
Arg. of periapsis
197.13°
True anomaly
178.62213°
Mean anomaly
178.5948°
Eccentric anomaly
178.6085°
Mean motion
3.14265 °/min
Orbital period
114.55 mins
BSTAR
0.00019836
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Other satellites on launch #70 in the year 1965 (1965-09-03 UTC)

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