Skip to content
Home Library Satellite Directory MOLNIYA 3-8

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
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
2362 km
Apogee
37977 km
Inclination
63.8°
Period
717.5 min
Mean Motion
2.00709193 rev/day
TLE Epoch
2026-06-17 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,170 km
Orbital Velocity13,951 km/h
Velocity3.88 km/s
Orbital Period11 hours 57 minutes
Orbits / Day2.01
Eccentricity0.6710
Semi-Major Axis26,541 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 2,362 km and 37,977 km with an inclination of 63.8°. It travels at approximately 13,951 km/h (3.88 km/s), completing one full orbit every 11 hours 57 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.6710 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 orbits at an average altitude of 20,170 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 3-8’s average altitude, there are currently 103 active payloads and 14 tracked debris or rocket body fragments — notable neighbours include GPS BIIR-5 (PRN 22), GPS BIIR-8 (PRN 16), GPS BIIR-11 (PRN 19). With an inclination of 63.8°, MOLNIYA 3-8 passes over latitudes between 63.8°N and 63.8°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, of which 56 share a similar altitude band with MOLNIYA 3-8.
❓ Frequently Asked Questions
MOLNIYA 3-8 orbits in Medium Earth Orbit (MEO) at altitudes between 2,362 km (perigee) and 37,977 km (apogee), with an average altitude of approximately 20,170 km. It completes one orbit every 11 hours 57 minutes, travelling at approximately 13,951 km/h (8,669 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 or browse all operators in the operator directory.
MOLNIYA 3-8 was launched on 1977-10-28 from PKMTR. View the full satellite launch log.
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. You can also browse the satellite directory to find other tracked objects.
MOLNIYA 3-8 travels at approximately 13,951 km/h (8,669 mph) — roughly 3.88 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.