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ARTEMIS

NORAD 26863 Payload GEO 2001-029A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36009 km
Apogee
36116 km
Inclination
14.8°
Period
1450.2 min
Mean Motion
0.99295178 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,063 km
Orbital Velocity11,034 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0013
Semi-Major Axis42,434 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
2001-07-12
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2001-029A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ARTEMIS is an active satellite operated by ESA (European Space Agency), launched on 2001-07-12 from Guiana Space Centre, Kourou. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,009 km and 36,116 km with an inclination of 14.8°. It travels at approximately 11,034 km/h (3.06 km/s), completing one full orbit every 24.2 hours — that’s roughly 0.99 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 ARTEMIS in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ARTEMIS 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 14.8°, 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 ARTEMIS’s average altitude, there are currently 120 active payloads and 22 tracked debris or rocket body fragments. ESA (European Space Agency) operates approximately 93 active satellites in total, of which 3 share a similar altitude band with ARTEMIS.
❓ Frequently Asked Questions
ARTEMIS orbits at approximately 36,063 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 11,034 km/h — it just keeps pace with the ground below. With an inclination of 14.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ARTEMIS is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26863. You can track ARTEMIS in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ARTEMIS was launched on 2001-07-12 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. View the full satellite launch log.
Yes — Orbital Radar tracks ARTEMIS (NORAD ID 26863) 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.
ARTEMIS travels at approximately 11,034 km/h (6,856 mph) — roughly 3.06 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.