JCSAT 1
NORAD 19874
Payload
GEO
1989-020A
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GEO · NORAD 19874
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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
35985 km
Apogee
36007 km
Inclination
14.8°
Period
1446.8 min
Mean Motion
0.99530315 rev/day
TLE Epoch
2026-06-18 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,996 km
Orbital Velocity11,042 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0003
Semi-Major Axis42,367 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 SKY Perfect JSAT (Japan)
Launch Date
1989-03-06
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1989-020A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
JCSAT 1 is an active satellite operated by SKY Perfect JSAT (Japan), launched on 1989-03-06 from Guiana Space Centre, Kourou. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,985 km and 36,007 km with an inclination of 14.8°. It travels at approximately 11,042 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 JCSAT 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
JCSAT 1 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 JCSAT 1’s average altitude, there are currently 58 active payloads and 29 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 5 share a similar altitude band with JCSAT 1.
❓ Frequently Asked Questions
JCSAT 1 orbits at approximately 35,996 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 11,042 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.
JCSAT 1 is operated by SKY Perfect JSAT (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 19874. You can track JCSAT 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
JCSAT 1 was launched on 1989-03-06 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 JCSAT 1 (NORAD ID 19874) 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.
JCSAT 1 travels at approximately 11,042 km/h (6,861 mph) — roughly 3.07 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.