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: 20 hours ago

TLE from 20 hours ago
0 SL-8 R/B
1 01575U 65070F   26048.44413276 -.00000117  00000-0 -12000-3 0  9994
2 01575  56.1240  78.4887 0097197 279.4327 194.9545 12.57013214775706
Epoch: 2026-02-17T10:39Z
TLE epoch observation values (Epoch: 2026-02-17T10:39:33.070Z)
Latitude
49.40037°
Longitude
-100.03678°
Altitude
1,514.794 km
Speed
7.079 km/s
True Right ascension
13h 49m 06s
True Declination
49° 14' 48"
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
09:14:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,511.053 km
Perigee altitude
1,359.168 km
Semi-major axis
7,813.247 km
Eccentricity
0.00972
Inclination
56.124°
RAAN
78.4887°
Arg. of periapsis
279.4327°
True anomaly
194.67042°
Mean anomaly
194.9545°
Eccentric anomaly
194.81213°
Mean motion
3.14265 °/min
Orbital period
114.55 mins
BSTAR
-0.00012
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Other satellites on launch #70 in the year 1965 (1965-09-03 UTC)

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