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: 17 hours ago
TLE from 17 hours ago
0 SL-8 R/B
1 02802U 67045B 25292.25671594 .00000822 00000-0 23519-3 0 9998
2 02802 74.0098 252.1905 0065655 293.1942 66.2309 14.45472393 68588Epoch: 2025-10-19T06:09Z
TLE epoch observation values (Epoch: 2025-10-19T06:09:40.257Z)
Latitude
-0°
Longitude
131.79678°
Altitude
724.513 km
Speed
7.503 km/s
True Right ascension
16h 48m 45s
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
18:11:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
784.812 km
Perigee altitude
691.369 km
Semi-major axis
7,116.227 km
Eccentricity
0.00657
Inclination
74.0098°
RAAN
252.1905°
Arg. of periapsis
293.1942°
True anomaly
66.9217°
Mean anomaly
66.2309°
Eccentric anomaly
66.57607°
Mean motion
3.6155 °/min
Orbital period
99.57 mins
BSTAR
0.00023519
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-20 07:37:31.875Z | 8.304° NNE | 2025-10-20 07:41:31.875Z | 59.102° ENE | 21.877° | 2025-10-20 07:45:31.875Z | 111.037° ESE |
| 8 mins | 2025-10-20 09:19:31.875Z | 321.682° NNW | 2025-10-20 09:23:31.875Z | 248.06° W | 34.357° | 2025-10-20 09:27:31.875Z | 189.856° SSW |
| 8 mins | 2025-10-20 22:09:31.875Z | 176.437° S | 2025-10-20 22:12:31.875Z | 118.494° SE | 39.932° | 2025-10-20 22:17:31.875Z | 27.922° NE |
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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