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MOLNIYA 1-S

NORAD 7392 Payload GEO 1974-060A ● Active
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🛰️ Orbital Parameters
Perigee
35763 km
Apogee
35838 km
Inclination
1.1°
Period
1436.8 min
Mean Motion
1.00222315 rev/day
TLE Epoch
2026-10-21 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,801 km
Orbital Velocity11,068 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0009
Semi-Major Axis42,172 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 GUKOS RVSN (Russia (CIS))
Launch Date
1974-07-29
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1974-060A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-S is an active satellite operated by GUKOS RVSN (Russia (CIS)), launched on 1974-07-29 from Baikonur Cosmodrome, Kazakhstan on the Molniya-1 11F658 No. 38 launch. After more than 52 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,763 km and 35,838 km with an inclination of 1.1°. It travels at approximately 11,068 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks MOLNIYA 1-S 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-S occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 1.1°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of MOLNIYA 1-S’s average altitude, there are currently 737 active payloads and 64 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Russia (CIS) operates approximately 1,553 active satellites in total, of which 128 share a similar altitude band with MOLNIYA 1-S.
❓ Frequently Asked Questions
MOLNIYA 1-S orbits at approximately 35,801 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,068 km/h — it just keeps pace with the ground below. With an inclination of 1.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
MOLNIYA 1-S is operated by GUKOS RVSN (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 7392. You can track MOLNIYA 1-S in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-S was launched on 1974-07-29 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks MOLNIYA 1-S (NORAD ID 7392) 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-S travels at approximately 11,068 km/h (6,877 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.