SL-8 R/B, 3048
Orbit data source: Space-Track
SL-8 R/B, 3048 is space debris in LEO originally from a launch on Thu, 23 Nov 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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3048 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: 11 hours ago
TLE from 11 hours ago
0 SL-8 R/B
1 03048U 67116B 25305.41899861 .00000908 00000-0 18284-3 0 9990
2 03048 74.0050 287.0171 0005550 98.6340 17.0689 14.63076520 72727Epoch: 2025-11-01T10:03Z
TLE epoch observation values (Epoch: 2025-11-01T10:03:21.479Z)
Latitude
60.10798°
Longitude
-114.50595°
Altitude
689.386 km
Speed
7.52 km/s
True Right ascension
05h 09m 07s
True Declination
59° 57' 28"
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
16:39:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
684.772 km
Perigee altitude
676.937 km
Semi-major axis
7,058.991 km
Eccentricity
0.00056
Inclination
74.005°
RAAN
287.0171°
Arg. of periapsis
98.634°
True anomaly
17.08758°
Mean anomaly
17.0689°
Eccentric anomaly
17.07824°
Mean motion
3.65956 °/min
Orbital period
98.37 mins
BSTAR
0.00018284
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Other satellites on launch #116 in the year 1967 (1967-11-23 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-02 00:26:45.522Z | 216.132° SW | 2025-11-02 00:29:45.522Z | 299.415° NW | 41.306° | 2025-11-02 00:33:45.522Z | 10.661° NNE |
| 4 mins | 2025-11-02 09:04:45.522Z | 33.38° NE | 2025-11-02 09:06:45.522Z | 65.445° ENE | 18.019° | 2025-11-02 09:08:45.522Z | 94.597° ESE |
| 7 mins | 2025-11-02 10:43:45.522Z | 320.713° NNW | 2025-11-02 10:46:45.522Z | 260.032° W | 35.058° | 2025-11-02 10:50:45.522Z | 187.479° SSW |
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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