MOLNIYA 3-8
NORAD 10455
Payload
MEO
1977-105A
● Active
CONNECTING…
MEO · NORAD 10455
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
2338 km
Apogee
38019 km
Inclination
63.8°
Period
717.8 min
Mean Motion
2.00627617 rev/day
TLE Epoch
2026-05-08 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,179 km
Orbital Velocity13,949 km/h
Velocity3.87 km/s
Orbital Period11 hours 58 minutes
Orbits / Day2.01
Eccentricity0.6720
Semi-Major Axis26,550 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1977-10-28
Launch Site
PKMTR
Int'l Designator
1977-105A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 3-8 is an active satellite operated by Russia (CIS), launched on 1977-10-28 from PKMTR. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,338 km and 38,019 km with an inclination of 63.8°. It travels at approximately 13,949 km/h (3.87 km/s), completing one full orbit every 11 hours 58 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.6720 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 3-8 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 3-8 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 3-8 orbits in Medium Earth Orbit (MEO) at altitudes between 2,338 km (perigee) and 38,019 km (apogee), with an average altitude of approximately 20,179 km. It completes one orbit every 11 hours 58 minutes, travelling at approximately 13,949 km/h (8,668 mph).
MOLNIYA 3-8 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10455. You can track MOLNIYA 3-8 in real time on Orbital Radar’s live tracker.
MOLNIYA 3-8 was launched on 1977-10-28 from PKMTR.
Yes — Orbital Radar tracks MOLNIYA 3-8 (NORAD ID 10455) 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 3-8 travels at approximately 13,949 km/h (8,668 mph) — roughly 3.87 km/s. It completes 2.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.