ELEKTRON 1
NORAD 746
Payload
MEO
1964-006A
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
403 km
Apogee
6207 km
Inclination
60.9°
Period
158.1 min
Mean Motion
9.11069129 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,305 km
Orbital Velocity23,106 km/h
Velocity6.42 km/s
Orbital Period2 hours 38 minutes
Orbits / Day9.11
Eccentricity0.2999
Semi-Major Axis9,676 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 OKB-1 (Russia (CIS))
Launch Date
1964-01-30
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1964-006A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ELEKTRON 1 is an active satellite operated by OKB-1 (Russia (CIS)), launched on 1964-01-30 from Baikonur Cosmodrome, Kazakhstan on the 2D No. 1 launch. After more than 62 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 403 km and 6,207 km with an inclination of 60.9°. It travels at approximately 23,106 km/h (6.42 km/s), completing one full orbit every 2 hours 38 minutes — that’s roughly 9.11 orbits per day. Its orbital eccentricity of 0.2999 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks ELEKTRON 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ELEKTRON 1 orbits at an average altitude of 3,305 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 ELEKTRON 1’s average altitude, there are currently 3 active payloads and 6 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 60.9°, ELEKTRON 1 passes over latitudes between 60.9°N and 60.9°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 1,553 active satellites in total.
❓ Frequently Asked Questions
ELEKTRON 1 orbits in Medium Earth Orbit (MEO) at altitudes between 403 km (perigee) and 6,207 km (apogee), with an average altitude of approximately 3,305 km. It completes one orbit every 2 hours 38 minutes, travelling at approximately 23,106 km/h (14,357 mph).
ELEKTRON 1 is operated by OKB-1 (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 746. You can track ELEKTRON 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ELEKTRON 1 was launched on 1964-01-30 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. 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 ELEKTRON 1 (NORAD ID 746) 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.
ELEKTRON 1 travels at approximately 23,106 km/h (14,357 mph) — roughly 6.42 km/s. It completes 9.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 18 sunrises and sunsets every 24 hours.