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ISO

NORAD 23715 Payload HEO 1995-062A ● Active
CONNECTING… HEO · NORAD 23715
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
493 km
Apogee
70015 km
Inclination
1.2°
Period
1409.0 min
Mean Motion
1.02200865 rev/day
TLE Epoch
2026-06-18 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,254 km
Orbital Velocity11,140 km/h
Velocity3.09 km/s
Orbital Period23 hours 29 minutes
Orbits / Day1.02
Eccentricity0.8351
Semi-Major Axis41,625 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1995-11-17
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1995-062A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ISO is an active satellite operated by ESA (European Space Agency), launched on 1995-11-17 from Guiana Space Centre, Kourou. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 493 km and 70,015 km with an inclination of 1.2°. It travels at approximately 11,140 km/h (3.09 km/s), completing one full orbit every 23 hours 29 minutes — that’s roughly 1.02 orbits per day. Its orbital eccentricity of 0.8351 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 ISO in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ISO follows a Highly Elliptical Orbit, sweeping between 493 km (perigee) and 70,015 km (apogee). It spends most of its 23 hours 29 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. Within ±50 km of ISO’s average altitude, there are currently 3 active payloads and 14 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 1.2°, ISO passes over latitudes between 1.2°N and 1.2°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. ESA (European Space Agency) operates approximately 93 active satellites in total.
❓ Frequently Asked Questions
ISO follows a Highly Elliptical Orbit, swinging between 493 km (perigee) and 70,015 km (apogee). It spends most of its 23 hours 29 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
ISO is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23715. You can track ISO in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ISO was launched on 1995-11-17 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: permanent — geostationary orbit, no atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks ISO (NORAD ID 23715) 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.
ISO’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 11,140 km/h (3.09 km/s), completing one revolution every 23 hours 29 minutes. Learn more about highly elliptical orbits.