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MOLNIYA 3-42

NORAD 22178 Payload MEO 1992-067A ● Active
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1231 km
Apogee
35892 km
Inclination
64.5°
Period
653.3 min
Mean Motion
2.20433920 rev/day
TLE Epoch
2026-03-12 00:00:00 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
Eccentricity0.6951
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)
🔗 Constellation / Groups
geo protected plus
📖 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 1,231 km and 35,892 km with an inclination of 64.5°. 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 0.6951 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Geo Protected Plus constellation group. 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 operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.
❓ Frequently Asked Questions
MOLNIYA 3-42 orbits in Medium Earth Orbit (MEO) at altitudes between 1,231 km (perigee) and 35,892 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.
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.
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.
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.
MOLNIYA 3-42 is a member of the Geo Protected Plus constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geo Protected Plus satellites on Orbital Radar’s live tracker.