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MOLNIYA 1-86

NORAD 22671 Payload MEO 1993-035A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
351 km
Apogee
13505 km
Inclination
62.9°
Period
254.6 min
Mean Motion
5.65632303 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude6,928 km
Orbital Velocity19,709 km/h
Velocity5.47 km/s
Orbital Period4 hours 15 minutes
Orbits / Day5.66
Eccentricity0.4945
Semi-Major Axis13,299 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1993-05-26
Launch Site
PKMTR
Int'l Designator
1993-035A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-86 is an active satellite operated by Russia (CIS), launched on 1993-05-26 from PKMTR. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 351 km and 13,505 km with an inclination of 62.9°. It travels at approximately 19,709 km/h (5.47 km/s), completing one full orbit every 4 hours 15 minutes — that’s roughly 5.66 orbits per day. Its orbital eccentricity of 0.4945 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-86 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 1-86 orbits at an average altitude of 6,928 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 1-86’s average altitude, there are currently 1 active payload and 3 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 62.9°, MOLNIYA 1-86 passes over latitudes between 62.9°N and 62.9°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 1,285 active satellites in total.
❓ Frequently Asked Questions
MOLNIYA 1-86 orbits in Medium Earth Orbit (MEO) at altitudes between 351 km (perigee) and 13,505 km (apogee), with an average altitude of approximately 6,928 km. It completes one orbit every 4 hours 15 minutes, travelling at approximately 19,709 km/h (12,247 mph).
MOLNIYA 1-86 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22671. You can track MOLNIYA 1-86 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-86 was launched on 1993-05-26 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 1-86 (NORAD ID 22671) 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 1-86 travels at approximately 19,709 km/h (12,247 mph) — roughly 5.47 km/s. It completes 5.66 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 11 sunrises and sunsets every 24 hours.