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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
836 km
Apogee
39538 km
Inclination
63.1°
Period
718.2 min
Mean Motion
2.00509231 rev/day
TLE Epoch
2026-03-13 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,187 km
Orbital Velocity13,947 km/h
Velocity3.87 km/s
Orbital Period11 hours 58 minutes
Orbits / Day2.01
Eccentricity0.7286
Semi-Major Axis26,558 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)
🔗 Constellation / Groups
geo protected plus
📖 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 836 km and 39,538 km with an inclination of 63.1°. It travels at approximately 13,947 km/h (3.87 km/s), completing one full orbit every 11 hours 58 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.7286 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Geo Protected Plus constellation group. 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 operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.
❓ Frequently Asked Questions
MOLNIYA 1-63 orbits in Medium Earth Orbit (MEO) at altitudes between 836 km (perigee) and 39,538 km (apogee), with an average altitude of approximately 20,187 km. It completes one orbit every 11 hours 58 minutes, travelling at approximately 13,947 km/h (8,666 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.
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.
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.
MOLNIYA 1-63 travels at approximately 13,947 km/h (8,666 mph) — roughly 3.87 km/s. It completes 2.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.
MOLNIYA 1-63 is a member of the Geo Protected Plus constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geo Protected Plus satellites on Orbital Radar’s live tracker.