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MOLNIYA 3-42

NORAD 22178 Payload MEO 1992-067A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1145 km
Apogee
35978 km
Inclination
64.4°
Period
653.3 min
Mean Motion
2.20432148 rev/day
TLE Epoch
2026-06-18 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude18,562 km
Orbital Velocity14,394 km/h
Velocity4.00 km/s
Orbital Period10 hours 53 minutes
Orbits / Day2.20
Eccentricity0.6985
Semi-Major Axis24,933 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1992-10-14
Launch Site
PKMTR
Int'l Designator
1992-067A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 3-42 is an active satellite operated by Russia (CIS), launched on 1992-10-14 from PKMTR. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,145 km and 35,978 km with an inclination of 64.4°. It travels at approximately 14,394 km/h (4.00 km/s), completing one full orbit every 10 hours 53 minutes — that’s roughly 2.20 orbits per day. Its orbital eccentricity of 0.6985 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 3-42 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 3-42 orbits at an average altitude of 18,562 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 3-42’s average altitude, there are currently 1 active payload and 13 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 64.4°, MOLNIYA 3-42 passes over latitudes between 64.4°N and 64.4°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 3-42 orbits in Medium Earth Orbit (MEO) at altitudes between 1,145 km (perigee) and 35,978 km (apogee), with an average altitude of approximately 18,562 km. It completes one orbit every 10 hours 53 minutes, travelling at approximately 14,394 km/h (8,944 mph).
MOLNIYA 3-42 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22178. You can track MOLNIYA 3-42 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 3-42 was launched on 1992-10-14 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 3-42 (NORAD ID 22178) 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 3-42 travels at approximately 14,394 km/h (8,944 mph) — roughly 4.00 km/s. It completes 2.20 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.