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MOLNIYA 1-80

NORAD 21118 Payload MEO 1991-012A ● Active
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🛰️ Orbital Parameters
Perigee
3151 km
Apogee
36402 km
Inclination
64.9°
Period
701.6 min
Mean Motion
2.05246779 rev/day
TLE Epoch
2026-11-01 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,777 km
Orbital Velocity14,056 km/h
Velocity3.90 km/s
Orbital Period11 hours 42 minutes
Orbits / Day2.05
Eccentricity0.6358
Semi-Major Axis26,148 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 UNKS RF (Russia (CIS))
Launch Date
1991-02-15
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1991-012A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-80 is an active satellite operated by UNKS RF (Russia (CIS)), launched on 1991-02-15 from Plesetsk Cosmodrome, Russia on the Molniya-1T No. 73? launch. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,151 km and 36,402 km with an inclination of 64.9°. It travels at approximately 14,056 km/h (3.90 km/s), completing one full orbit every 11 hours 42 minutes — that’s roughly 2.05 orbits per day. Its orbital eccentricity of 0.6358 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-80 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 1-80 orbits at an average altitude of 19,777 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 1-80’s average altitude, there are currently 1 active payload and 17 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 64.9°, MOLNIYA 1-80 passes over latitudes between 64.9°N and 64.9°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 1,548 active satellites in total.
❓ Frequently Asked Questions
MOLNIYA 1-80 orbits in Medium Earth Orbit (MEO) at altitudes between 3,151 km (perigee) and 36,402 km (apogee), with an average altitude of approximately 19,777 km. It completes one orbit every 11 hours 42 minutes, travelling at approximately 14,056 km/h (8,734 mph).
MOLNIYA 1-80 is operated by UNKS RF (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21118. You can track MOLNIYA 1-80 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-80 was launched on 1991-02-15 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. View the full satellite launch log.
Yes — Orbital Radar tracks MOLNIYA 1-80 (NORAD ID 21118) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 1-80 travels at approximately 14,056 km/h (8,734 mph) — roughly 3.90 km/s. It completes 2.05 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.