SL-4 DEB, 68757 (Decayed)
Orbit data source: Space-Track
SL-4 DEB, 68757 was space debris in LEO originally from a launch on Thu, 16 Apr 2026 UTC via a SOYUZ-2-1B launch vehicle 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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68757 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed spacecraft
Bus & Motor
UNK, Unknown motor
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 SL-4 DEB
1 68757U 26083E 26195.96554465 .13365978 29541-5 64818-2 0 9996
2 68757 98.2108 352.8025 0018139 291.0661 68.8686 16.20759226 13720Epoch: 2026-07-14T23:10Z
TLE epoch observation values (Epoch: 2026-07-14T23:10:23.057Z)
Latitude
-0.00002°
Longitude
72.3783°
Altitude
216.396 km
Speed
7.779 km/s
True Right ascension
23h 31m 12s
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
11:51:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
226.32 km
Perigee altitude
202.404 km
Semi-major axis
6,592.499 km
Eccentricity
0.00181
Inclination
98.2108°
RAAN
352.8025°
Arg. of periapsis
291.0661°
True anomaly
69.06264°
Mean anomaly
68.8686°
Eccentric anomaly
68.9656°
Mean motion
4.05479 °/min
Orbital period
88.78 mins
BSTAR
0.0064818
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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
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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