SL-4 R/B, 62906 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 62906 was space debris in LEO originally from a launch on Wed, 05 Feb 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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62906 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed spacecraft
Bus & Motor
BLOK-I, Unknown motor
Mass
Wet unknown, 2,350 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 3.5 m
Radar Cross Section
17.919 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 SL-4 R/B
1 62906U 25026E 25083.14126979 .15542753 -14596-5 14981-3 0 9994
2 62906 81.9679 166.0817 0040249 247.4325 195.2930 16.47297977 7409Epoch: 2025-03-24T03:23Z
TLE epoch observation values (Epoch: 2025-03-24T03:23:25.709Z)
Latitude
79.15292°
Longitude
-19.56409°
Altitude
185.071 km
Speed
7.787 km/s
True Right ascension
14h 12m 37s
True Declination
79° 05' 01"
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
11:06:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
169.536 km
Perigee altitude
117.04 km
Semi-major axis
6,521.425 km
Eccentricity
0.00402
Inclination
81.9679°
RAAN
166.0817°
Arg. of periapsis
247.4325°
True anomaly
195.17194°
Mean anomaly
195.293°
Eccentric anomaly
195.23241°
Mean motion
4.12125 °/min
Orbital period
87.35 mins
BSTAR
0.00014981
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Other satellites on launch #26 in the year 2025 (2025-02-05 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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