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COSMOS 1989 (ETALON 1)

NORAD 19751 Payload MEO 1989-001C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
19066 km
Apogee
19185 km
Inclination
64.9°
Period
675.6 min
Mean Motion
2.13156033 rev/day
TLE Epoch
2026-03-17 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,126 km
Orbital Velocity14,234 km/h
Velocity3.95 km/s
Orbital Period11 hours 16 minutes
Orbits / Day2.13
Eccentricity0.0023
Semi-Major Axis25,497 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1989-01-10
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1989-001C
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
geodetic
📖 About This Object
COSMOS 1989 (ETALON 1) is an active satellite operated by Russia (CIS), launched on 1989-01-10 from Baikonur, Kazakhstan. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 19,066 km and 19,185 km with an inclination of 64.9°. It travels at approximately 14,234 km/h (3.95 km/s), completing one full orbit every 11 hours 16 minutes — that’s roughly 2.13 orbits per day. It is part of the Geodetic constellation group. Orbital Radar tracks COSMOS 1989 (ETALON 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
COSMOS 1989 (ETALON 1) operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.
❓ Frequently Asked Questions
COSMOS 1989 (ETALON 1) orbits in Medium Earth Orbit (MEO) at altitudes between 19,066 km (perigee) and 19,185 km (apogee), with an average altitude of approximately 19,126 km. It completes one orbit every 11 hours 16 minutes, travelling at approximately 14,234 km/h (8,845 mph).
COSMOS 1989 (ETALON 1) is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 19751. You can track COSMOS 1989 (ETALON 1) in real time on Orbital Radar’s live tracker.
COSMOS 1989 (ETALON 1) was launched on 1989-01-10 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan.
Yes — Orbital Radar tracks COSMOS 1989 (ETALON 1) (NORAD ID 19751) 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.
COSMOS 1989 (ETALON 1) travels at approximately 14,234 km/h (8,845 mph) — roughly 3.95 km/s. It completes 2.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.
COSMOS 1989 (ETALON 1) is a member of the Geodetic constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geodetic satellites on Orbital Radar’s live tracker.