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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

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<iframe src="https://www.satcat.com/sats-embedded/10365?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/10365?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

10365, 1977-092A

Orbit

GEO

Last TLE update

23 hours ago

Origin

MinSvyazi SSR Soyuzniy Uzel Radioveshchaniya i Radiosvyazi No. 9 (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 (48 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 23 hours ago

0 EKRAN 2
1 10365U 77092A   25129.10717442  .00000085  00000-0  00000-0 0  9998
2 10365   5.2727 280.0677 0034606   9.2565  30.6576  1.00301648130808

Epoch: 2025-05-09T02:34Z

Definitive object data (Epoch: 2025-05-09T02:34:19.869Z)

Latitude

3.41966°

Longitude

54.30278°

Altitude

35,652.694 km

Speed

3.084 km/s

True Right ascension

21h 20m 12s

True Declination

3° 24' 58"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

2.5174°

Longitude

42.4844°

Altitude

35,640.021 km

Speed

3.085 km/s

Apparent Right ascension

20h 41m 23s

Apparent Declination

-2° 44' 11"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

09:55:04

Azimuth

28.913° NE

Elevation

-49.243°

Doppler factor

Orbital elements

Apogee altitude

35,925.173 km

Perigee altitude

35,633.393 km

Semi-major axis

42,157.42 km

Eccentricity

0.0034606

Inclination

5.2727°

RAAN

280.0677°

Arg. of periapsis

9.2565°

True anomaly

30.86056°

Mean anomaly

30.6576°

Eccentric anomaly

30.759°

Mean motion

0.25074 °/min

BSTAR

Unknown

Orbital period

1435.72 mins

Loading historical data...

10365 neighbors

Authenticating...

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Other satellites on launch #92 in the year 1977 (1977-09-20 UTC)

SL-12 R/B(1), 10366 (Decayed)

SL-12 PLAT, 10367 (Decayed)

SL-12 DEB, 10368 (Decayed)

SL-12 R/B(AUX MOTOR), 10408 (Decayed)

SL-12 R/B(AUX MOTOR), 10484 (Decayed)

EKRAN 2 Visibility forecast

Observer location: undefined°, undefined°

EKRAN 2 is not visible in the next 10 days

Authenticating...

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Check out EKRAN 2, 10365 on other resources

View EKRAN 2, 10365 on NASA - NSSDCA Website

View EKRAN 2, 10365 on Heavens-Above

View EKRAN 2, 10365 on Keep Track

View EKRAN 2, 10365 on Celestrak

View EKRAN 2, 10365 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.