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AMSAT OSCAR 40

NORAD 26609 Payload HEO 2000-072B ● Active
CONNECTING… HEO · NORAD 26609
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1129 km
Apogee
58691 km
Inclination
9.4°
Period
1146.6 min
Mean Motion
1.25588322 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude29,910 km
Orbital Velocity11,933 km/h
Velocity3.31 km/s
Orbital Period19 hours 7 minutes
Orbits / Day1.26
Eccentricity0.7933
Semi-Major Axis36,281 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇩🇪 Germany
Launch Date
2000-11-16
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2000-072B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AMSAT OSCAR 40 is an active satellite operated by Germany, launched on 2000-11-16 from Guiana Space Centre, Kourou. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 1,129 km and 58,691 km with an inclination of 9.4°. It travels at approximately 11,933 km/h (3.31 km/s), completing one full orbit every 19 hours 7 minutes — that’s roughly 1.26 orbits per day. Its orbital eccentricity of 0.7933 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks AMSAT OSCAR 40 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AMSAT OSCAR 40 follows a Highly Elliptical Orbit, sweeping between 1,129 km (perigee) and 58,691 km (apogee). It spends most of its 19 hours 7 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 9.4°, AMSAT OSCAR 40 passes over latitudes between 9.4°N and 9.4°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Germany operates approximately 80 active satellites in total.
❓ Frequently Asked Questions
AMSAT OSCAR 40 follows a Highly Elliptical Orbit, swinging between 1,129 km (perigee) and 58,691 km (apogee). It spends most of its 19 hours 7 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
AMSAT OSCAR 40 is operated by Germany. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26609. You can track AMSAT OSCAR 40 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AMSAT OSCAR 40 was launched on 2000-11-16 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks AMSAT OSCAR 40 (NORAD ID 26609) 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.
AMSAT OSCAR 40’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 11,933 km/h (3.31 km/s), completing one revolution every 19 hours 7 minutes. Learn more about highly elliptical orbits.