Skip to content
Home › Library › Satellite Directory › COSMOS 637

COSMOS 637

NORAD 7229 Payload GEO 1974-017A ● Active
CONNECTING… GEO · NORAD 7229
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35483 km
Apogee
35804 km
Inclination
0.5°
Period
1428.8 min
Mean Motion
1.00785493 rev/day
TLE Epoch
2026-10-21 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,644 km
Orbital Velocity11,088 km/h
Velocity3.08 km/s
Orbital Period23 hours 49 minutes
Orbits / Day1.01
Eccentricity0.0038
Semi-Major Axis42,015 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 OKB-10 (Russia (CIS))
Launch Date
1974-03-26
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1974-017A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
COSMOS 637 is an active satellite operated by OKB-10 (Russia (CIS)), launched on 1974-03-26 from Baikonur Cosmodrome, Kazakhstan on the 11F638 GVM launch. After more than 52 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,483 km and 35,804 km with an inclination of 0.5°. It travels at approximately 11,088 km/h (3.08 km/s), completing one full orbit every 23 hours 49 minutes — that’s roughly 1.01 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 637 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 637 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 0.5°, 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 637’s average altitude, there are currently 11 active payloads and 24 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,553 active satellites in total, of which 2 share a similar altitude band with COSMOS 637.
❓ Frequently Asked Questions
COSMOS 637 orbits at approximately 35,644 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 11,088 km/h — it just keeps pace with the ground below. With an inclination of 0.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
COSMOS 637 is operated by OKB-10 (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 7229. You can track COSMOS 637 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
COSMOS 637 was launched on 1974-03-26 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 637 (NORAD ID 7229) 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.
COSMOS 637 travels at approximately 11,088 km/h (6,890 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.