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EKRAN 2, 10365

Orbit data source: Space-Track

EKRAN 2, 10365 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Tue, 20 Sep 1977 UTC via a PROTON-K/DM launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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

EKRAN 2 details

Identifier	10365, 1977-092A
Orbit	GEO
Last TLE update	1 day ago
Origin	MSvyaz (CIS)
Manufacturer	NPO PM
Mission	Non-operational Civil Communications
Bus & Motor	EKRAN, Unknown motor
Mass	2,000 kg wet, ~1,850 kg dry
Launch date (UTC)	1977-09-20 (47 years ago)
Launch vehicle	PROTON-K/DM
Launch site	Tyuratam Missile And Space Complex (TTMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl + 2 Pan + 1 Plate, 9 m
Radar Cross Section	17.622 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 EKRAN 2
1 10365U 77092A   25035.19362521  .00000120  00000-0  00000-0 0  9997
2 10365   5.5135 281.2747 0043266   3.1860 330.1884  1.00264057129853

Epoch: 2025-02-04T04:38Z

Definitive object data (Epoch: 2025-02-04T04:38:49.218Z)

Latitude	-2.48896°
Longitude	50.22693°
Altitude	35,630.476 km
Speed	3.086 km/s
True Right ascension	16h 58m 08s
True Declination	-2° 29' 11"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	1.95924°
Longitude	97.85084°
Altitude	35,613.552 km
Speed	3.087 km/s
Apparent Right ascension	20h 18m 38s
Apparent Declination	-3° 14' 51"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:46:33
Azimuth	34.158° NE
Elevation	-48.285°
Doppler factor	1

Orbital elements

Apogee altitude	35,972.261 km
Perigee altitude	35,607.374 km
Semi-major axis	42,167.954 km
Eccentricity	0.0043266
Inclination	5.5135°
RAAN	281.2747°
Arg. of periapsis	3.186°
True anomaly	329.94076°
Mean anomaly	330.1884°
Eccentric anomaly	330.06469°
Mean motion	0.25065 °/min
BSTAR	Unknown
Orbital period	1436.26 mins