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MOLNIYA 1-62

NORAD 15214 Payload MEO 1984-089A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
983 km
Apogee
34797 km
Inclination
63.0°
Period
627.1 min
Mean Motion
2.29642462 rev/day
TLE Epoch
2026-06-17 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,890 km
Orbital Velocity14,592 km/h
Velocity4.05 km/s
Orbital Period10 hours 27 minutes
Orbits / Day2.30
Eccentricity0.6969
Semi-Major Axis24,261 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1984-08-24
Launch Site
PKMTR
Int'l Designator
1984-089A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-62 is an active satellite operated by Russia (CIS), launched on 1984-08-24 from PKMTR. With over 42 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 983 km and 34,797 km with an inclination of 63.0°. It travels at approximately 14,592 km/h (4.05 km/s), completing one full orbit every 10 hours 27 minutes — that’s roughly 2.30 orbits per day. Its orbital eccentricity of 0.6969 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-62 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 1-62 orbits at an average altitude of 17,890 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 1-62’s average altitude, there are currently 1 active payload and 20 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 63.0°, MOLNIYA 1-62 passes over latitudes between 63.0°N and 63.0°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 1,286 active satellites in total.
❓ Frequently Asked Questions
MOLNIYA 1-62 orbits in Medium Earth Orbit (MEO) at altitudes between 983 km (perigee) and 34,797 km (apogee), with an average altitude of approximately 17,890 km. It completes one orbit every 10 hours 27 minutes, travelling at approximately 14,592 km/h (9,067 mph).
MOLNIYA 1-62 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 15214. You can track MOLNIYA 1-62 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-62 was launched on 1984-08-24 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 1-62 (NORAD ID 15214) 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 1-62 travels at approximately 14,592 km/h (9,067 mph) — roughly 4.05 km/s. It completes 2.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.