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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2802 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
S3, Unknown motor
Mass
1,434 kg wet, 1,434 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 SL-8 R/B
1 2802U 67045B 25318.69447699 .00000682 00000-0 19626-3 0 9990
2 2802 74.0109 202.8289 0065401 238.3648 121.1119 14.45506301 72404Epoch: 2025-11-14T16:40Z
TLE epoch observation values (Epoch: 2025-11-14T16:40:02.811Z)
Latitude
-0.00005°
Longitude
-101.21712°
Altitude
767.266 km
Speed
7.458 km/s
True Right ascension
13h 31m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
20:18:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
784.519 km
Perigee altitude
691.439 km
Semi-major axis
7,116.116 km
Eccentricity
0.00654
Inclination
74.0109°
RAAN
202.8289°
Arg. of periapsis
238.3648°
True anomaly
121.75083°
Mean anomaly
121.1119°
Eccentric anomaly
121.43163°
Mean motion
3.61559 °/min
Orbital period
99.57 mins
BSTAR
0.00019626
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Other satellites on launch #45 in the year 1967 (1967-05-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SL-8 R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-15 03:11:29.767Z | 358.331° N | 2025-11-15 03:15:29.767Z | 55.722° ENE | 32.076° | 2025-11-15 03:20:29.767Z | 133.88° SE |
| 6 mins | 2025-11-15 04:54:29.767Z | 299.715° NW | 2025-11-15 04:56:29.767Z | 270.815° WNW | 21.029° | 2025-11-15 05:00:29.767Z | 214.366° SW |
| 9 mins | 2025-11-15 17:42:29.767Z | 203.856° SW | 2025-11-15 17:46:29.767Z | 256.002° W | 44.048° | 2025-11-15 17:51:29.767Z | 15.603° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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