DECAYED

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.

Not visible in the next 10 days
Identifier
62906, 2025-026E
Orbit
Decayed
Last TLE update
2 months ago
Origin
Manufacturer
TsSKB-Progress
Mission
Decayed spacecraft
Bus & Motor
BLOK-I, Unknown motor
Mass
Wet unknown, 2,350 kg dry
Launch date (UTC)
2025-02-05 (3 months ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 7.1 m
Radar Cross Section
17.919 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 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  7409
Epoch: 2025-03-24T03:23Z
Definitive object data (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
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
169.536 km
Perigee altitude
117.04 km
Semi-major axis
6,521.425 km
Eccentricity
0.0040249
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
BSTAR
0.00014981
Orbital period
87.35 mins
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Other satellites on launch #26 in the year 2025 (2025-02-05 UTC)

SL-4 R/B Visibility forecast

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This satellite is decayed
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