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MOLNIYA 1-91

NORAD 25485 Payload MEO 1998-054A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1562 km
Apogee
33282 km
Inclination
64.7°
Period
609.0 min
Mean Motion
2.36442301 rev/day
TLE Epoch
2026-06-19 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,422 km
Orbital Velocity14,735 km/h
Velocity4.09 km/s
Orbital Period10 hours 9 minutes
Orbits / Day2.36
Eccentricity0.6666
Semi-Major Axis23,793 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1998-09-28
Launch Site
PKMTR
Int'l Designator
1998-054A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-91 is an active satellite operated by Russia (CIS), launched on 1998-09-28 from PKMTR. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,562 km and 33,282 km with an inclination of 64.7°. It travels at approximately 14,735 km/h (4.09 km/s), completing one full orbit every 10 hours 9 minutes — that’s roughly 2.36 orbits per day. Its orbital eccentricity of 0.6666 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-91 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 1-91 orbits at an average altitude of 17,422 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 1-91’s average altitude, there are currently 2 active payloads and 12 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 64.7°, MOLNIYA 1-91 passes over latitudes between 64.7°N and 64.7°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.
❓ Frequently Asked Questions
MOLNIYA 1-91 orbits in Medium Earth Orbit (MEO) at altitudes between 1,562 km (perigee) and 33,282 km (apogee), with an average altitude of approximately 17,422 km. It completes one orbit every 10 hours 9 minutes, travelling at approximately 14,735 km/h (9,156 mph).
MOLNIYA 1-91 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25485. You can track MOLNIYA 1-91 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-91 was launched on 1998-09-28 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 1-91 (NORAD ID 25485) 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 1-91 travels at approximately 14,735 km/h (9,156 mph) — roughly 4.09 km/s. It completes 2.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.