COSMOS 2536, 44422 (Decayed)

Orbit data source: Space-Track

COSMOS 2536, 44422 was a payload satellite owned by TsNIIKhM (CIS) in LEO that was launched on Wed, 10 Jul 2019 UTC via a SOYUZ-2-1V launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

COSMOS 2536 details

Identifier	44422, 2019-039B
Orbit	Decayed
Last TLE update	6 months ago
Origin	TsNIIKhM (CIS)
Manufacturer	TsNIIKhM
Mission	Decayed Defense Technology
Bus & Motor	NAPRAZHENIYE?, Unknown motor
Mass	~47 kg wet, ~47 kg dry
Launch date (UTC)	2019-07-10 (5 years ago)
Launch vehicle	SOYUZ-2-1V
Launch site	Plesetsk Missile And Space Complex (PKMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Hex Cyl + 1 Ant, 1 m
Radar Cross Section	0.352 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 6 months ago

0 COSMOS 2536
1 44422U 19039B   24173.43098059  .28361618  26373-5  35843-2 0  9999
2 44422  97.6230 232.2810 0018306 264.6712 219.3930 16.35442729269927

Epoch: 2024-06-21T10:20Z

Definitive object data (Epoch: 2024-06-21T10:20:36.722Z)

Latitude	55.43291°
Longitude	-1.84508°
Altitude	196.528 km
Speed	7.788 km/s
True Right ascension	04h 13m 40s
True Declination	55° 15' 30"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	186.773 km
Perigee altitude	162.782 km
Semi-major axis	6,552.914 km
Eccentricity	0.0018306
Inclination	97.623°
RAAN	232.281°
Arg. of periapsis	264.6712°
True anomaly	219.26011°
Mean anomaly	219.393°
Eccentric anomaly	219.32653°
Mean motion	4.09158 °/min
BSTAR	0.0035843
Orbital period	87.99 mins