INTELSAT 26 (JCSAT 4)
NORAD 24732
Payload
GEO
1997-007A
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GEO · NORAD 24732
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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
36133 km
Apogee
36216 km
Inclination
12.3°
Period
1455.9 min
Mean Motion
0.98904812 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,175 km
Orbital Velocity11,019 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0010
Semi-Major Axis42,546 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Intelsat (ITSO)
Launch Date
1997-02-17
Launch Site
Cape Canaveral, Florida
Int'l Designator
1997-007A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
intelsat
📖 About This Object
INTELSAT 26 (JCSAT 4) is an active satellite operated by Intelsat (ITSO), launched on 1997-02-17 from Cape Canaveral, Florida. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,133 km and 36,216 km with an inclination of 12.3°. It travels at approximately 11,019 km/h (3.06 km/s), completing one full orbit every 24.3 hours — that’s roughly 0.99 orbits per day. It is part of the Intelsat constellation group. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks INTELSAT 26 (JCSAT 4) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
INTELSAT 26 (JCSAT 4) 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 12.3°, 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 INTELSAT 26 (JCSAT 4)’s average altitude, there are currently 150 active payloads and 11 tracked debris or rocket body fragments. ITSO operates approximately 72 active satellites in total, of which 15 share a similar altitude band with INTELSAT 26 (JCSAT 4).
🔗 Intelsat Communications
This satellite is operated by Intelsat, one of the pioneering commercial satellite operators, with a fleet of 50+ geostationary satellites providing television distribution, enterprise networking, mobility connectivity and government communications worldwide. Intelsat was founded in 1964 as an intergovernmental organisation and privatised in 2001.
❓ Frequently Asked Questions
INTELSAT 26 (JCSAT 4) orbits at approximately 36,175 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 11,019 km/h — it just keeps pace with the ground below. With an inclination of 12.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INTELSAT 26 (JCSAT 4) is operated by Intelsat (ITSO). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24732. You can track INTELSAT 26 (JCSAT 4) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INTELSAT 26 (JCSAT 4) was launched on 1997-02-17 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks INTELSAT 26 (JCSAT 4) (NORAD ID 24732) 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.
INTELSAT 26 (JCSAT 4) travels at approximately 11,019 km/h (6,847 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.
INTELSAT 26 (JCSAT 4) is a member of the Intelsat constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Intelsat satellites on Orbital Radar’s live tracker.