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MOLNIYA 2-10, 7376

Orbit data source: Space-Track

MOLNIYA 2-10, 7376 is a payload satellite owned by GUKOS RVSN (CIS) in HEO that was launched on Tue, 23 Jul 1974 UTC via an MOLNIYA 8K78M launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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.

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https://www.satcat.com/sats-embedded/7376?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

7376, 1974-056A

Orbit

HEO

Last TLE update

4 days ago

Origin

Main Directorate of Ministry of Foreign Affairs (CIS)

Manufacturer

OKB-10

Mission

Defense Communications

Bus & Motor

MOLNIYA-2, Unknown motor

Mass

~1,650 kg wet, ~1,620 kg dry

Launch date (UTC)

1974-07-23 (51 years ago)

Launch vehicle

MOLNIYA 8K78M

Launch site

Plesetsk Missile And Space Complex (PKMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 6 Pan, 8.2 m

Radar Cross Section

15.101 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 4 days ago

0 MOLNIYA 2-10
1 07376U 74056A   25125.96951051 -.00001005  00000-0  00000-0 0  9993
2 07376  65.3671 342.3313 6822562 274.8844  16.5360  2.01086917371545

Epoch: 2025-05-05T23:16Z

Definitive object data (Epoch: 2025-05-05T23:16:05.708Z)

Latitude

-0.00029°

Longitude

129.28533°

Altitude

7,043.084 km

Speed

6.661 km/s

True Right ascension

22h 49m 32s

True Declination

0° 00' 01"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

32.71775°

Longitude

-68.23153°

Altitude

19,366.727 km

Speed

3.992 km/s

Apparent Right ascension

10h 31m 37s

Apparent Declination

25° 17' 45"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:46:33

Azimuth

72.183° E

Elevation

18.622°

Doppler factor

Orbital elements

Apogee altitude

38,223.935 km

Perigee altitude

2,046.282 km

Semi-major axis

26,513.246 km

Eccentricity

0.6822562

Inclination

65.3671°

RAAN

342.3313°

Arg. of periapsis

274.8844°

True anomaly

84.94244°

Mean anomaly

16.536°

Eccentric anomaly

43.38914°

Mean motion

0.50275 °/min

BSTAR

Unknown

Orbital period

716.07 mins

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Other satellites on launch #56 in the year 1974 (1974-07-23 UTC)

SL-6 R/B(1), 7377 (Decayed)

SL-6 PLAT, 7378 (Decayed)

SL-6 R/B(2), 7382 (Decayed)

MOLNIYA 2-10 Visibility forecast

Observer location: undefined°, undefined°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
23 mins	2025-05-09 20:35:24.134Z	72.21° E	2025-05-09 20:35:24.134Z	72.21° E	17.703°	2025-05-09 20:58:24.134Z	81.353° E
393 mins	2025-05-10 00:54:24.134Z	325.922° NNW	2025-05-10 04:24:24.134Z	330.659° NNW	21.541°	2025-05-10 07:27:24.134Z	315.952° NNW
576 mins	2025-05-10 10:59:24.134Z	92.782° ESE	2025-05-10 13:43:24.134Z	38.694° NE	30.728°	2025-05-10 20:35:24.134Z	74.616° E

Authenticating...

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Check out MOLNIYA 2-10, 7376 on other resources

View MOLNIYA 2-10, 7376 on NASA - NSSDCA Website

View MOLNIYA 2-10, 7376 on Heavens-Above

View MOLNIYA 2-10, 7376 on Keep Track

View MOLNIYA 2-10, 7376 on Celestrak

View MOLNIYA 2-10, 7376 on Gunter's Space Page

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