ELEKTRO-L 2
NORAD 41105
Payload
GEO
2015-074A
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GEO · NORAD 41105
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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
35783 km
Apogee
35791 km
Inclination
6.7°
Period
1436.1 min
Mean Motion
1.00270556 rev/day
TLE Epoch
2026-06-18 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0001
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Roshydromet - Planeta (Russia (CIS))
Launch Date
2015-12-11
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2015-074A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ELEKTRO-L 2 is an active satellite operated by Roshydromet - Planeta (Russia (CIS)), launched on 2015-12-11 from Baikonur, Kazakhstan. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,783 km and 35,791 km with an inclination of 6.7°. It travels at approximately 11,070 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 ELEKTRO-L 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ELEKTRO-L 2 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 6.7°, 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 ELEKTRO-L 2’s average altitude, there are currently 713 active payloads and 59 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Russia (CIS) operates approximately 1,286 active satellites in total, of which 124 share a similar altitude band with ELEKTRO-L 2.
❓ Frequently Asked Questions
ELEKTRO-L 2 orbits at approximately 35,787 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 11,070 km/h — it just keeps pace with the ground below. With an inclination of 6.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ELEKTRO-L 2 is operated by Roshydromet - Planeta (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 41105. You can track ELEKTRO-L 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ELEKTRO-L 2 was launched on 2015-12-11 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks ELEKTRO-L 2 (NORAD ID 41105) 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.
ELEKTRO-L 2 travels at approximately 11,070 km/h (6,878 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.