MOLNIYA 2-10
NORAD 7376
Payload
MEO
1974-056A
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
2457 km
Apogee
37798 km
Inclination
65.2°
Period
715.8 min
Mean Motion
2.01181794 rev/day
TLE Epoch
2026-10-20 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,128 km
Orbital Velocity13,962 km/h
Velocity3.88 km/s
Orbital Period11 hours 56 minutes
Orbits / Day2.01
Eccentricity0.6668
Semi-Major Axis26,499 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 GUKOS RVSN (Russia (CIS))
Launch Date
1974-07-23
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1974-056A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 2-10 is an active satellite operated by GUKOS RVSN (Russia (CIS)), launched on 1974-07-23 from Plesetsk Cosmodrome, Russia on the Molniya-2 launch. After more than 52 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,457 km and 37,798 km with an inclination of 65.2°. It travels at approximately 13,962 km/h (3.88 km/s), completing one full orbit every 11 hours 56 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.6668 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 2-10 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MOLNIYA 2-10 orbits at an average altitude of 20,128 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of MOLNIYA 2-10’s average altitude, there are currently 40 active payloads and 17 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 65.2°, MOLNIYA 2-10 passes over latitudes between 65.2°N and 65.2°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Russia (CIS) operates approximately 1,552 active satellites in total, of which 34 share a similar altitude band with MOLNIYA 2-10.
❓ Frequently Asked Questions
MOLNIYA 2-10 orbits in Medium Earth Orbit (MEO) at altitudes between 2,457 km (perigee) and 37,798 km (apogee), with an average altitude of approximately 20,128 km. It completes one orbit every 11 hours 56 minutes, travelling at approximately 13,962 km/h (8,676 mph).
MOLNIYA 2-10 is operated by GUKOS RVSN (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 7376. You can track MOLNIYA 2-10 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 2-10 was launched on 1974-07-23 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. View the full satellite launch log.
Yes — Orbital Radar tracks MOLNIYA 2-10 (NORAD ID 7376) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
MOLNIYA 2-10 travels at approximately 13,962 km/h (8,676 mph) — roughly 3.88 km/s. It completes 2.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.