SL-8 R/B, 2802

Orbit data source: Space-Track

SL-8 R/B, 2802 is space debris in LEO originally from a launch on Mon, 15 May 1967 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
2802, 1967-045B
Orbit
LEO
Last TLE update
10 hours ago
Origin
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
S3, Unknown motor
Mass
1,434 kg wet, 1,434 kg dry
Launch date (UTC)
1967-05-15 (58 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

TLE from 10 hours ago
0 SL-8 R/B
1 02802U 67045B   25199.58226178  .00000213  00000-0  66673-4 0  9997
2 02802  74.0109  65.2174 0063771 129.6436 231.0373 14.45390268 55196
Epoch: 2025-07-18T13:58Z
TLE epoch observation values (Epoch: 2025-07-18T13:58:27.417Z)
Latitude
-0.00009°
Longitude
-81.02852°
Altitude
772.091 km
Speed
7.453 km/s
True Right ascension
04h 20m 52s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-21.11005°
Longitude
-88.11297°
Altitude
787.873 km
Speed
7.438 km/s
Apparent Right ascension
02h 31m 14s
Apparent Declination
-32° 05' 29"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:38:01
Azimuth
280.043° WNW
Elevation
-65.923°
Doppler factor
1
Orbital elements
Apogee altitude
783.743 km
Perigee altitude
692.977 km
Semi-major axis
7,116.497 km
Eccentricity
0.00638
Inclination
74.0109°
RAAN
65.2174°
Arg. of periapsis
129.6436°
True anomaly
230.47194°
Mean anomaly
231.0373°
Eccentric anomaly
230.75433°
Mean motion
3.6153 °/min
Orbital period
99.58 mins
BSTAR
0.000066673
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Other satellites on launch #45 in the year 1967 (1967-05-15 UTC)
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