COSMOS 1408, 13552 (Decayed)

Orbit data source: Space-Track

COSMOS 1408, 13552 was a payload satellite owned by GRU (CIS) in LEO that was launched on Thu, 16 Sep 1982 UTC via a TSIKLON-3 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 1408 details

Identifier	13552, 1982-092A
Orbit	Decayed
Last TLE update	2 months ago
Origin	GRU (CIS)
Manufacturer	Yuzhnoe
Mission	Decayed Defense Sigint
Bus & Motor	TSELINA-D, Unknown motor
Mass	1,750 kg wet, 1,750 kg dry
Launch date (UTC)	1982-09-16 (42 years ago)
Launch vehicle	TSIKLON-3
Launch site	Plesetsk Missile And Space Complex (PKMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl + 1 Ant, 13.14 m
Radar Cross Section	13.217 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 months ago

0 COSMOS 1408
1 13552U 82092A   24301.23445417  .15659680 -12246-5  27896-3 0  9993
2 13552  82.5280  99.1133 0006890 255.2900 160.8321 16.47511674309572

Epoch: 2024-10-27T05:37Z

Definitive object data (Epoch: 2024-10-27T05:37:36.84Z)

Latitude	55.53948°
Longitude	-10.41456°
Altitude	159.465 km
Speed	7.813 km/s
True Right ascension	07h 20m 16s
True Declination	55° 21' 51"
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	147.19 km
Perigee altitude	138.205 km
Semi-major axis	6,520.834 km
Eccentricity	0.000689
Inclination	82.528°
RAAN	99.1133°
Arg. of periapsis	255.29°
True anomaly	160.858°
Mean anomaly	160.8321°
Eccentric anomaly	160.84505°
Mean motion	4.12181 °/min
BSTAR	0.00027896
Orbital period	87.34 mins