MOLNIYA 3-20
NORAD 13875
Payload
MEO
1983-015A
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MEO · NORAD 13875
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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
1234 km
Apogee
39117 km
Inclination
62.0°
Period
717.7 min
Mean Motion
2.00660851 rev/day
TLE Epoch
2026-09-16 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,176 km
Orbital Velocity13,950 km/h
Velocity3.87 km/s
Orbital Period11 hours 58 minutes
Orbits / Day2.01
Eccentricity0.7135
Semi-Major Axis26,547 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 NPO PM / MSvyaz (Russia (CIS))
Launch Date
1983-03-11
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1983-015A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 3-20 is an active satellite operated by NPO PM / MSvyaz (Russia (CIS)), launched on 1983-03-11 from Plesetsk Cosmodrome, Russia on the Molniya-3 No. 34 launch. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,234 km and 39,117 km with an inclination of 62.0°. It travels at approximately 13,950 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 0.7135 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 3-20 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 3-20 orbits at an average altitude of 20,176 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 3-20’s average altitude, there are currently 103 active payloads and 14 tracked debris or rocket body fragments. With an inclination of 62.0°, MOLNIYA 3-20 passes over latitudes between 62.0°N and 62.0°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 1,536 active satellites in total, of which 54 share a similar altitude band with MOLNIYA 3-20.
❓ Frequently Asked Questions
MOLNIYA 3-20 orbits in Medium Earth Orbit (MEO) at altitudes between 1,234 km (perigee) and 39,117 km (apogee), with an average altitude of approximately 20,176 km. It completes one orbit every 11 hours 58 minutes, travelling at approximately 13,950 km/h (8,668 mph).
MOLNIYA 3-20 is operated by NPO PM / MSvyaz (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13875. You can track MOLNIYA 3-20 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 3-20 was launched on 1983-03-11 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. 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 3-20 (NORAD ID 13875) 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 3-20 travels at approximately 13,950 km/h (8,668 mph) — roughly 3.87 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.