INTEGRAL
NORAD 27540
Payload
HEO
2002-048A
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HEO · NORAD 27540
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
4185 km
Apogee
145287 km
Inclination
89.9°
Period
3831.8 min
Mean Motion
0.37579950 rev/day
TLE Epoch
2026-06-17 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude74,736 km
Orbital Velocity7,981 km/h
Velocity2.22 km/s
Orbital Period63.9 hours
Orbits / Day0.38
Eccentricity0.8699
Semi-Major Axis81,107 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
European Space Operations Centre (ESOC)/NASA/Russia (ESA (European Space Agency))
Launch Date
2002-10-17
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2002-048A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INTEGRAL is an active satellite operated by European Space Operations Centre (ESOC)/NASA/Russia (ESA (European Space Agency)), launched on 2002-10-17 from Baikonur, Kazakhstan. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 4,185 km and 145,287 km with an inclination of 89.9°. It travels at approximately 7,981 km/h (2.22 km/s), completing one full orbit every 63.9 hours — that’s roughly 0.38 orbits per day. Its orbital eccentricity of 0.8699 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks INTEGRAL in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
INTEGRAL follows a Highly Elliptical Orbit, sweeping between 4,185 km (perigee) and 145,287 km (apogee). It spends most of its 63.9 hours 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 89.9°, INTEGRAL passes over latitudes between 89.9°N and 89.9°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. ESA (European Space Agency) operates approximately 93 active satellites in total.
❓ Frequently Asked Questions
INTEGRAL follows a Highly Elliptical Orbit, swinging between 4,185 km (perigee) and 145,287 km (apogee). It spends most of its 63.9 hours orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
INTEGRAL is operated by European Space Operations Centre (ESOC)/NASA/Russia (ESA (European Space Agency)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27540. You can track INTEGRAL in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INTEGRAL was launched on 2002-10-17 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 INTEGRAL (NORAD ID 27540) 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.
INTEGRAL’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 7,981 km/h (2.22 km/s), completing one revolution every 63.9 hours. Learn more about highly elliptical orbits.