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MOLNIYA 1-63

NORAD 15429 Payload MEO 1984-124A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
819 km
Apogee
39586 km
Inclination
63.0°
Period
718.8 min
Mean Motion
2.00335116 rev/day
TLE Epoch
2026-06-19 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,203 km
Orbital Velocity13,943 km/h
Velocity3.87 km/s
Orbital Period11 hours 59 minutes
Orbits / Day2.00
Eccentricity0.7294
Semi-Major Axis26,574 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1984-12-14
Launch Site
PKMTR
Int'l Designator
1984-124A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-63 is an active satellite operated by Russia (CIS), launched on 1984-12-14 from PKMTR. With over 42 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 819 km and 39,586 km with an inclination of 63.0°. It travels at approximately 13,943 km/h (3.87 km/s), completing one full orbit every 11 hours 59 minutes — that’s roughly 2.00 orbits per day. Its orbital eccentricity of 0.7294 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-63 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 1-63 orbits at an average altitude of 20,203 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 1-63’s average altitude, there are currently 99 active payloads and 17 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 63.0°, MOLNIYA 1-63 passes over latitudes between 63.0°N and 63.0°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 52 share a similar altitude band with MOLNIYA 1-63.
❓ Frequently Asked Questions
MOLNIYA 1-63 orbits in Medium Earth Orbit (MEO) at altitudes between 819 km (perigee) and 39,586 km (apogee), with an average altitude of approximately 20,203 km. It completes one orbit every 11 hours 59 minutes, travelling at approximately 13,943 km/h (8,664 mph).
MOLNIYA 1-63 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 15429. You can track MOLNIYA 1-63 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-63 was launched on 1984-12-14 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 1-63 (NORAD ID 15429) 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 1-63 travels at approximately 13,943 km/h (8,664 mph) — roughly 3.87 km/s. It completes 2.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.