SL-4 R/B, 67235 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 67235 was space debris in LEO originally from a launch on Thu, 25 Dec 2025 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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67235 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed spacecraft
Bus & Motor
BLOK-I, Unknown motor
Mass
~0 kg wet, 2,350 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
21.560 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 SL-4 R/B
1 67235U 25310B 26077.48002462 .11109380 28275-5 13469-3 0 9990
2 67235 97.9206 99.2198 0023010 127.9666 342.5783 16.48041047 13055Epoch: 2026-03-18T11:31Z
TLE epoch observation values (Epoch: 2026-03-18T11:31:14.127Z)
Latitude
68.20651°
Longitude
-49.39251°
Altitude
141.998 km
Speed
7.836 km/s
True Right ascension
19h 57m 50s
True Declination
68° 04' 35"
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
10:19:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.322 km
Perigee altitude
126.319 km
Semi-major axis
6,519.458 km
Eccentricity
0.0023
Inclination
97.9206°
RAAN
99.2198°
Arg. of periapsis
127.9666°
True anomaly
342.49914°
Mean anomaly
342.5783°
Eccentric anomaly
342.53874°
Mean motion
4.12312 °/min
Orbital period
87.31 mins
BSTAR
0.00013469
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Other satellites on launch #310 in the year 2025 (2025-12-25 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-4 R/B Visibility
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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. |
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| This satellite is decayed. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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