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 (61 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: 20 hours ago

TLE from 20 hours ago
0 SL-8 R/B
1 01575U 65070F   26138.44974642 -.00000112  00000-0 -82671-4 0  9990
2 01575  56.1225 192.8029 0100567  42.0030 331.2044 12.57010773787024
Epoch: 2026-05-18T10:47Z
TLE epoch observation values (Epoch: 2026-05-18T10:47:38.090Z)
Latitude
10.45476°
Longitude
161.83736°
Altitude
1,366.953 km
Speed
7.208 km/s
True Right ascension
13h 19m 32s
True Declination
10° 23' 54"
Sunlit
Object was in full shadow 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
15:53:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,513.696 km
Perigee altitude
1,356.545 km
Semi-major axis
7,813.258 km
Eccentricity
0.01006
Inclination
56.1225°
RAAN
192.8029°
Arg. of periapsis
42.003°
True anomaly
330.64313°
Mean anomaly
331.2044°
Eccentric anomaly
330.92438°
Mean motion
3.14264 °/min
Orbital period
114.55 mins
BSTAR
-0.000082671
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Other satellites on launch #70 in the year 1965 (1965-09-03 UTC)

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