PALAPA C2
NORAD 23864
Payload
GEO
1996-030A
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GEO · NORAD 23864
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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
36119 km
Apogee
36175 km
Inclination
11.7°
Period
1454.5 min
Mean Motion
0.98999793 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,147 km
Orbital Velocity11,023 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0007
Semi-Major Axis42,518 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Indonesia
Launch Date
1996-05-16
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1996-030A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
PALAPA C2 is an active satellite operated by Indonesia, launched on 1996-05-16 from Guiana Space Centre, Kourou. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,119 km and 36,175 km with an inclination of 11.7°. It travels at approximately 11,023 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 PALAPA C2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PALAPA C2 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 11.7°, 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 PALAPA C2’s average altitude, there are currently 172 active payloads and 9 tracked debris or rocket body fragments. Indonesia operates approximately 17 active satellites in total, of which 2 share a similar altitude band with PALAPA C2.
❓ Frequently Asked Questions
PALAPA C2 orbits at approximately 36,147 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 11,023 km/h — it just keeps pace with the ground below. With an inclination of 11.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
PALAPA C2 is operated by Indonesia. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23864. You can track PALAPA C2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PALAPA C2 was launched on 1996-05-16 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 PALAPA C2 (NORAD ID 23864) 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.
PALAPA C2 travels at approximately 11,023 km/h (6,849 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.