MOLNIYA 1-53
NORAD 13070
Payload
MEO
1982-015A
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MEO · NORAD 13070
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
1234 km
Apogee
39072 km
Inclination
64.0°
Period
716.8 min
Mean Motion
2.00892910 rev/day
TLE Epoch
2026-11-01 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,153 km
Orbital Velocity13,956 km/h
Velocity3.88 km/s
Orbital Period11 hours 57 minutes
Orbits / Day2.01
Eccentricity0.7133
Semi-Major Axis26,524 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 GUKOS (Russia (CIS))
Launch Date
1982-02-26
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1982-015A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOLNIYA 1-53 is an active satellite operated by GUKOS (Russia (CIS)), launched on 1982-02-26 from Plesetsk Cosmodrome, Russia on the Molniya-1 launch. With over 44 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,234 km and 39,072 km with an inclination of 64.0°. It travels at approximately 13,956 km/h (3.88 km/s), completing one full orbit every 11 hours 57 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.7133 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MOLNIYA 1-53 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 1-53 orbits at an average altitude of 20,153 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 1-53’s average altitude, there are currently 101 active payloads and 13 tracked debris or rocket body fragments. With an inclination of 64.0°, MOLNIYA 1-53 passes over latitudes between 64.0°N and 64.0°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 1,547 active satellites in total, of which 54 share a similar altitude band with MOLNIYA 1-53.
❓ Frequently Asked Questions
MOLNIYA 1-53 orbits in Medium Earth Orbit (MEO) at altitudes between 1,234 km (perigee) and 39,072 km (apogee), with an average altitude of approximately 20,153 km. It completes one orbit every 11 hours 57 minutes, travelling at approximately 13,956 km/h (8,672 mph).
MOLNIYA 1-53 is operated by GUKOS (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13070. You can track MOLNIYA 1-53 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOLNIYA 1-53 was launched on 1982-02-26 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 1-53 (NORAD ID 13070) 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 1-53 travels at approximately 13,956 km/h (8,672 mph) — roughly 3.88 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.