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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). Payload-class satellites include a variety of spacecraft 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
Identifier
10365, 1977-092A
Orbit
GEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO PM
Mission
Non-operational spacecraft
Bus & Motor
EKRAN, Unknown motor
Mass
2,000 kg wet, ~1,850 kg dry
Launch date (UTC)
1977-09-20 (48 years ago)
Launch vehicle
PROTON-K/DM
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 EKRAN 2
1 10365U 77092A   25307.60229383 -.00000194  00000-0  00000+0 0  9994
2 10365   4.8189 277.7120 0042031 358.6700  69.2265  1.00321741132591
Epoch: 2025-11-03T14:27Z
TLE epoch observation values (Epoch: 2025-11-03T14:27:18.186Z)
Latitude
4.50495°
Longitude
86.01796°
Altitude
35,710.177 km
Speed
3.08 km/s
True Right ascension
23h 03m 46s
True Declination
4° 30' 01"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:07:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,950.824 km
Perigee altitude
35,596.488 km
Semi-major axis
42,151.793 km
Eccentricity
0.0042
Inclination
4.8189°
RAAN
277.712°
Arg. of periapsis
358.67°
True anomaly
69.67766°
Mean anomaly
69.2265°
Eccentric anomaly
69.452°
Mean motion
0.2508 °/min
Orbital period
1,435.43 mins
BSTAR
0
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