COSMOS 2397
NORAD 27775
Payload
GEO
2003-015A
● Active
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GEO · NORAD 27775
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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
35557 km
Apogee
35907 km
Inclination
12.8°
Period
1433.3 min
Mean Motion
1.00466869 rev/day
TLE Epoch
2026-09-18 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,732 km
Orbital Velocity11,077 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0042
Semi-Major Axis42,103 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 PVO (Russia (CIS))
Launch Date
2003-04-24
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
2003-015A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
COSMOS 2397 is an active satellite operated by PVO (Russia (CIS)), launched on 2003-04-24 from Baikonur Cosmodrome, Kazakhstan on the Oko-1 No. 7126 launch. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,557 km and 35,907 km with an inclination of 12.8°. It travels at approximately 11,077 km/h (3.08 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 COSMOS 2397 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
COSMOS 2397 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 12.8°, 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 COSMOS 2397’s average altitude, there are currently 66 active payloads and 36 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,536 active satellites in total, of which 29 share a similar altitude band with COSMOS 2397.
🔗 Cosmos (Military/Government) Series
This satellite carries the Cosmos designation, used by Russia (and formerly the Soviet Union) as a generic identifier for military and government spacecraft. The Cosmos series encompasses reconnaissance, signals intelligence (SIGINT), early warning, navigation, communications and scientific payloads. Many Cosmos satellites have classified missions with limited publicly available information.
❓ Frequently Asked Questions
COSMOS 2397 orbits at approximately 35,732 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 11,077 km/h — it just keeps pace with the ground below. With an inclination of 12.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
COSMOS 2397 is operated by PVO (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27775. You can track COSMOS 2397 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
COSMOS 2397 was launched on 2003-04-24 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 2397 (NORAD ID 27775) 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.
COSMOS 2397 travels at approximately 11,077 km/h (6,883 mph) — roughly 3.08 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.