COSMOS 2543, 44835 (Decayed)

Orbit data source: Space-Track

COSMOS 2543, 44835 was a payload satellite owned by TsNIIKhM (CIS) in LEO that was launched on Mon, 25 Nov 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 2543 details

Identifier	44835, 2019-079D
Orbit	Decayed
Last TLE update	3 months ago
Origin	TsNIIKhM (CIS)
Manufacturer	TsNIIKhM
Mission	Decayed Defense Technology
Bus & Motor	NIVELIR, Unknown motor
Mass	~100 kg wet, ~100 kg dry
Launch date (UTC)	2019-11-25 (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, Unknown HBR
Radar Cross Section	0.352 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 months ago

0 COSMOS 2543
1 44835U 19079D   24239.08914493  .13719927  28148-5  11897-3 0  9994
2 44835  97.7078  12.4018 0012883 266.2390  93.7441 16.51465352261386

Epoch: 2024-08-26T02:08Z

Definitive object data (Epoch: 2024-08-26T02:08:22.121Z)

Latitude	-0.0001°
Longitude	5.48507°
Altitude	139.295 km
Speed	7.822 km/s
True Right ascension	00h 49m 36s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow 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	140.674 km
Perigee altitude	123.899 km
Semi-major axis	6,510.424 km
Eccentricity	0.0012883
Inclination	97.7078°
RAAN	12.4018°
Arg. of periapsis	266.239°
True anomaly	93.8914°
Mean anomaly	93.7441°
Eccentric anomaly	93.81775°
Mean motion	4.1317 °/min
BSTAR	0.00011897
Orbital period	87.13 mins