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: 3 hours ago

TLE from 3 hours ago
0 SL-8 R/B
1  1575U 65070F   26037.21213534 -.00000069  00000-0  16662-3 0  9995
2  1575  56.1245 109.1498 0097114 263.8722 127.7586 12.57013621774290
Epoch: 2026-02-06T05:05Z
TLE epoch observation values (Epoch: 2026-02-06T05:05:28.493Z)
Latitude
26.55886°
Longitude
-84.0639°
Altitude
1,483.644 km
Speed
7.103 km/s
True Right ascension
08h 34m 37s
True Declination
26° 26' 03"
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
10:37:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,510.986 km
Perigee altitude
1,359.231 km
Semi-major axis
7,813.246 km
Eccentricity
0.00971
Inclination
56.1245°
RAAN
109.1498°
Arg. of periapsis
263.8722°
True anomaly
128.63188°
Mean anomaly
127.7586°
Eccentric anomaly
128.19589°
Mean motion
3.14265 °/min
Orbital period
114.55 mins
BSTAR
0.00016662
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Other satellites on launch #70 in the year 1965 (1965-09-03 UTC)

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