MOLNIYA 1-56
NORAD 13890
Payload
MEO
1983-019A
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MEO · NORAD 13890
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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
1622 km
Apogee
38845 km
Inclination
62.5°
Period
720.1 min
Mean Motion
1.99980927 rev/day
TLE Epoch
2026-06-17 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,234 km
Orbital Velocity13,935 km/h
Velocity3.87 km/s
Orbital Period12 hours
Orbits / Day2.00
Eccentricity0.6996
Semi-Major Axis26,605 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1983-03-16
Launch Site
PKMTR
Int'l Designator
1983-019A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-56 is an active satellite operated by Russia (CIS), launched on 1983-03-16 from PKMTR. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,622 km and 38,845 km with an inclination of 62.5°. It travels at approximately 13,935 km/h (3.87 km/s), completing one full orbit every 12 hours — that’s roughly 2.00 orbits per day. Its orbital eccentricity of 0.6996 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-56 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 1-56 orbits at an average altitude of 20,234 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 1-56’s average altitude, there are currently 21 active payloads and 17 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 62.5°, MOLNIYA 1-56 passes over latitudes between 62.5°N and 62.5°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, of which 19 share a similar altitude band with MOLNIYA 1-56.
❓ Frequently Asked Questions
MOLNIYA 1-56 orbits in Medium Earth Orbit (MEO) at altitudes between 1,622 km (perigee) and 38,845 km (apogee), with an average altitude of approximately 20,234 km. It completes one orbit every 12 hours, travelling at approximately 13,935 km/h (8,659 mph).
MOLNIYA 1-56 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13890. You can track MOLNIYA 1-56 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-56 was launched on 1983-03-16 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 1-56 (NORAD ID 13890) 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 1-56 travels at approximately 13,935 km/h (8,659 mph) — roughly 3.87 km/s. It completes 2.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.