SL-4 R/B, 62906

Orbit data source: Space-Track

SL-4 R/B, 62906 is 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	LEO
Last TLE update	14 hours ago
Origin	RVSN RF (CIS)
Manufacturer	TsSKB-Progress
Mission	Spacecraft
Bus & Motor	BLOK-I, Unknown motor
Mass	Wet unknown, 2,350 kg dry
Launch date (UTC)	2025-02-05 (1 month ago)
Launch vehicle	Unknown
Launch site	Plesetsk Missile And Space Complex (PKMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 14 hours ago

0 SL-4 R/B
1 62906U 25026E   25070.58694681  .00710175 -92854-6  62076-3 0  9999
2 62906  81.9929 181.3135 0150414 304.4874 182.2257 15.93763849  5388

Epoch: 2025-03-11T14:05Z

Definitive object data (Epoch: 2025-03-11T14:05:12.204Z)

Latitude	52.71478°
Longitude	-30.06183°
Altitude	400.687 km
Speed	7.617 km/s
True Right ascension	23h 22m 54s
True Declination	52° 32' 24"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-74.10912°
Longitude	130.39732°
Altitude	222.779 km
Speed	7.826 km/s
Apparent Right ascension	19h 51m 05s
Apparent Declination	-72° 28' 40"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	08:38:07
Azimuth	173.545° S
Elevation	-56.926°
Doppler factor	1

Orbital elements

Apogee altitude	388.934 km
Perigee altitude	188.378 km
Semi-major axis	6,666.793 km
Eccentricity	0.0150414
Inclination	81.9929°
RAAN	181.3135°
Arg. of periapsis	304.4874°
True anomaly	182.16°
Mean anomaly	182.2257°
Eccentric anomaly	182.19273°
Mean motion	3.9872 °/min
BSTAR	0.00062076
Orbital period	90.29 mins