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COSMOS 1700

NORAD 16199 Payload GEO 1985-102A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35757 km
Apogee
35794 km
Inclination
9.7°
Period
1435.5 min
Mean Motion
1.00312875 rev/day
TLE Epoch
2026-06-19 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,776 km
Orbital Velocity11,071 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0004
Semi-Major Axis42,147 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1985-10-25
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1985-102A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
COSMOS 1700 is an active satellite operated by Russia (CIS), launched on 1985-10-25 from Baikonur, Kazakhstan. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,757 km and 35,794 km with an inclination of 9.7°. It travels at approximately 11,071 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 1700 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 1700 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 9.7°, 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 COSMOS 1700’s average altitude, there are currently 705 active payloads and 56 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 123 share a similar altitude band with COSMOS 1700.
🔗 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 1700 orbits at approximately 35,776 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 11,071 km/h — it just keeps pace with the ground below. With an inclination of 9.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
COSMOS 1700 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 16199. You can track COSMOS 1700 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
COSMOS 1700 was launched on 1985-10-25 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 COSMOS 1700 (NORAD ID 16199) 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 1700 travels at approximately 11,071 km/h (6,879 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.