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MOLNIYA 3-10

NORAD 11057 Payload MEO 1978-095A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
942 km
Apogee
19286 km
Inclination
63.7°
Period
351.3 min
Mean Motion
4.09913737 rev/day
TLE Epoch
2026-06-17 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude10,114 km
Orbital Velocity17,702 km/h
Velocity4.92 km/s
Orbital Period5 hours 51 minutes
Orbits / Day4.10
Eccentricity0.5564
Semi-Major Axis16,485 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1978-10-13
Launch Site
PKMTR
Int'l Designator
1978-095A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 3-10 is an active satellite operated by Russia (CIS), launched on 1978-10-13 from PKMTR. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 942 km and 19,286 km with an inclination of 63.7°. It travels at approximately 17,702 km/h (4.92 km/s), completing one full orbit every 5 hours 51 minutes — that’s roughly 4.10 orbits per day. Its orbital eccentricity of 0.5564 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 3-10 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 3-10 orbits at an average altitude of 10,114 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 3-10’s average altitude, there are currently 1 active payload and 3 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 63.7°, MOLNIYA 3-10 passes over latitudes between 63.7°N and 63.7°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 1,286 active satellites in total.
❓ Frequently Asked Questions
MOLNIYA 3-10 orbits in Medium Earth Orbit (MEO) at altitudes between 942 km (perigee) and 19,286 km (apogee), with an average altitude of approximately 10,114 km. It completes one orbit every 5 hours 51 minutes, travelling at approximately 17,702 km/h (11,000 mph).
MOLNIYA 3-10 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 11057. You can track MOLNIYA 3-10 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 3-10 was launched on 1978-10-13 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks MOLNIYA 3-10 (NORAD ID 11057) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. 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 3-10 travels at approximately 17,702 km/h (11,000 mph) — roughly 4.92 km/s. It completes 4.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 sunrises and sunsets every 24 hours.