SL-4 R/B, 68838 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 68838 was space debris in LEO originally from a Commonwealth of Independent States-origin launch on Sat, 25 Apr 2026 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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68838 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
None
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 SL-4 R/B
1 68838U 26093B 26117.63842432 .08101162 12482-4 42104-3 0 9996
2 68838 51.6491 189.8262 0008279 80.4171 279.7792 16.42181963 288Epoch: 2026-04-27T15:19Z
TLE epoch observation values (Epoch: 2026-04-27T15:19:19.861Z)
Latitude
-0.00001°
Longitude
104.36822°
Altitude
159.861 km
Speed
7.812 km/s
True Right ascension
12h 39m 18s
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
19:17:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
165.944 km
Perigee altitude
155.117 km
Semi-major axis
6,538.668 km
Eccentricity
0.00083
Inclination
51.6491°
RAAN
189.8262°
Arg. of periapsis
80.4171°
True anomaly
279.68569°
Mean anomaly
279.7792°
Eccentric anomaly
279.73245°
Mean motion
4.10496 °/min
Orbital period
87.7 mins
BSTAR
0.00042104
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Other satellites on launch #93 in the year 2026 (2026-04-25 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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