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MOLNIYA 1-52

NORAD 13012 Payload MEO 1981-123A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
494 km
Apogee
39838 km
Inclination
61.7°
Period
717.3 min
Mean Motion
2.00742862 rev/day
TLE Epoch
2026-03-15 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,166 km
Orbital Velocity13,952 km/h
Velocity3.88 km/s
Orbital Period11 hours 57 minutes
Orbits / Day2.01
Eccentricity0.7413
Semi-Major Axis26,537 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1981-12-23
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1981-123A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
geo protected plus
📖 About This Object
MOLNIYA 1-52 is an active satellite operated by Russia (CIS), launched on 1981-12-23 from Baikonur, Kazakhstan. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 494 km and 39,838 km with an inclination of 61.7°. It travels at approximately 13,952 km/h (3.88 km/s), completing one full orbit every 11 hours 57 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.7413 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Geo Protected Plus constellation group. Orbital Radar tracks MOLNIYA 1-52 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 1-52 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 1-52 orbits in Medium Earth Orbit (MEO) at altitudes between 494 km (perigee) and 39,838 km (apogee), with an average altitude of approximately 20,166 km. It completes one orbit every 11 hours 57 minutes, travelling at approximately 13,952 km/h (8,670 mph).
MOLNIYA 1-52 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13012. You can track MOLNIYA 1-52 in real time on Orbital Radar’s live tracker.
MOLNIYA 1-52 was launched on 1981-12-23 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag.
Yes — Orbital Radar tracks MOLNIYA 1-52 (NORAD ID 13012) 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 1-52 travels at approximately 13,952 km/h (8,670 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.
MOLNIYA 1-52 is a member of the Geo Protected Plus constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geo Protected Plus satellites on Orbital Radar’s live tracker.