MOLNIYA 1-90
NORAD 24960
Payload
MEO
1997-054A
● Active
CONNECTING…
MEO · NORAD 24960
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
1700 km
Apogee
24554 km
Inclination
64.4°
Period
451.9 min
Mean Motion
3.18690799 rev/day
TLE Epoch
2026-09-17 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude13,127 km
Orbital Velocity16,277 km/h
Velocity4.52 km/s
Orbital Period7 hours 32 minutes
Orbits / Day3.19
Eccentricity0.5861
Semi-Major Axis19,498 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 VKS RVSN (Russia (CIS))
Launch Date
1997-09-24
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1997-054A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-90 is an active satellite operated by VKS RVSN (Russia (CIS)), launched on 1997-09-24 from Plesetsk Cosmodrome, Russia on the Molniya-1T No. 98 launch. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,700 km and 24,554 km with an inclination of 64.4°. It travels at approximately 16,277 km/h (4.52 km/s), completing one full orbit every 7 hours 32 minutes — that’s roughly 3.19 orbits per day. Its orbital eccentricity of 0.5861 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-90 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 1-90 orbits at an average altitude of 13,127 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 1-90’s average altitude, there are currently 1 active payload and 5 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 64.4°, MOLNIYA 1-90 passes over latitudes between 64.4°N and 64.4°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 1,536 active satellites in total.
❓ Frequently Asked Questions
MOLNIYA 1-90 orbits in Medium Earth Orbit (MEO) at altitudes between 1,700 km (perigee) and 24,554 km (apogee), with an average altitude of approximately 13,127 km. It completes one orbit every 7 hours 32 minutes, travelling at approximately 16,277 km/h (10,114 mph).
MOLNIYA 1-90 is operated by VKS RVSN (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24960. You can track MOLNIYA 1-90 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-90 was launched on 1997-09-24 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. 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 1-90 (NORAD ID 24960) 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 1-90 travels at approximately 16,277 km/h (10,114 mph) — roughly 4.52 km/s. It completes 3.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 sunrises and sunsets every 24 hours.