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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
931 km
Apogee
19297 km
Inclination
63.7°
Period
351.3 min
Mean Motion
4.09913163 rev/day
TLE Epoch
2026-05-08 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
Eccentricity0.5571
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 931 km and 19,297 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 0.5571 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 operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.
❓ Frequently Asked Questions
MOLNIYA 3-10 orbits in Medium Earth Orbit (MEO) at altitudes between 931 km (perigee) and 19,297 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.
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.
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.
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.
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