SL-4 DEB, 68755 (Decayed)
Orbit data source: Space-Track
SL-4 DEB, 68755 was space debris in SSO originally from a launch on Thu, 16 Apr 2026 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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68755 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
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 SL-4 DEB
1 68755U 26083C 26108.35291177 .22174759 36165-5 21653-2 0 9994
2 68755 98.2527 253.8385 0170194 68.7663 293.1699 16.05765192 223Epoch: 2026-04-18T08:28Z
TLE epoch observation values (Epoch: 2026-04-18T08:28:11.576Z)
Latitude
-0.00005°
Longitude
-79.6827°
Altitude
218.855 km
Speed
7.8 km/s
True Right ascension
16h 55m 21s
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
10:08:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
368.275 km
Perigee altitude
142.478 km
Semi-major axis
6,633.514 km
Eccentricity
0.01702
Inclination
98.2527°
RAAN
253.8385°
Arg. of periapsis
68.7663°
True anomaly
291.3621°
Mean anomaly
293.1699°
Eccentric anomaly
292.26748°
Mean motion
4.01724 °/min
Orbital period
89.61 mins
BSTAR
0.0021653
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Other satellites on launch #83 in the year 2026 (2026-04-16 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 DEB 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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