MOLNIYA 1-52
NORAD 13012
Payload
HEO
1981-123A
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HEO · NORAD 13012
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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
299 km
Apogee
40062 km
Inclination
61.9°
Period
717.9 min
Mean Motion
2.00597331 rev/day
TLE Epoch
2026-11-01 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,181 km
Orbital Velocity13,948 km/h
Velocity3.87 km/s
Orbital Period11 hours 58 minutes
Orbits / Day2.01
Eccentricity0.7488
Semi-Major Axis26,552 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 GUKOS (Russia (CIS))
Launch Date
1981-12-23
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1981-123A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-52 is an active satellite operated by GUKOS (Russia (CIS)), launched on 1981-12-23 from Baikonur Cosmodrome, Kazakhstan on the Molniya-1 11F658 No. 55 launch. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 299 km and 40,062 km with an inclination of 61.9°. It travels at approximately 13,948 km/h (3.87 km/s), completing one full orbit every 11 hours 58 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.7488 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 follows a Highly Elliptical Orbit, sweeping between 299 km (perigee) and 40,062 km (apogee). It spends most of its 11 hours 58 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of MOLNIYA 1-52’s average altitude, there are currently 104 active payloads and 12 tracked debris or rocket body fragments. With an inclination of 61.9°, MOLNIYA 1-52 passes over latitudes between 61.9°N and 61.9°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 1,547 active satellites in total, of which 55 share a similar altitude band with MOLNIYA 1-52.
❓ Frequently Asked Questions
MOLNIYA 1-52 follows a Highly Elliptical Orbit, swinging between 299 km (perigee) and 40,062 km (apogee). It spends most of its 11 hours 58 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
MOLNIYA 1-52 is operated by GUKOS (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 or browse all operators in the operator directory.
MOLNIYA 1-52 was launched on 1981-12-23 from Baikonur Cosmodrome, 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. View the full satellite launch log.
Yes — Orbital Radar tracks MOLNIYA 1-52 (NORAD ID 13012) 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 1-52’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 13,948 km/h (3.87 km/s), completing one revolution every 11 hours 58 minutes. Learn more about highly elliptical orbits.