SL-8 R/B, 3577

Orbit data source: Space-Track

SL-8 R/B, 3577 is space debris in LEO originally from a launch on Sat, 30 Nov 1968 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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
3577, 1968-106B
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)
1968-11-30 (57 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.1 m
Radar Cross Section
10.179 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 SL-8 R/B
1 03577U 68106B   25260.85119929  .00000163  00000-0  45769-3 0  9996
2 03577  74.0528  37.3517 0034183  76.7364  35.6404 13.19118137733480
Epoch: 2025-09-17T20:25Z
TLE epoch observation values (Epoch: 2025-09-17T20:25:43.618Z)
Latitude
62.67567°
Longitude
-119.48486°
Altitude
1,177.493 km
Speed
7.281 km/s
True Right ascension
12h 15m 52s
True Declination
62° 32' 35"
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
12:36:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,211.7 km
Perigee altitude
1,159.988 km
Semi-major axis
7,563.981 km
Eccentricity
0.00342
Inclination
74.0528°
RAAN
37.3517°
Arg. of periapsis
76.7364°
True anomaly
35.86944°
Mean anomaly
35.6404°
Eccentric anomaly
35.75484°
Mean motion
3.29927 °/min
Orbital period
109.12 mins
BSTAR
0.00045769
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Other satellites on launch #106 in the year 1968 (1968-11-30 UTC)

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