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PALAPA B4

NORAD 21964 Payload GEO 1992-027A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35869 km
Apogee
35891 km
Inclination
13.2°
Period
1440.9 min
Mean Motion
0.99939876 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,880 km
Orbital Velocity11,057 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0003
Semi-Major Axis42,251 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Indonesia
Launch Date
1992-05-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
1992-027A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
PALAPA B4 is an active satellite operated by Indonesia, launched on 1992-05-14 from Cape Canaveral, Florida. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,869 km and 35,891 km with an inclination of 13.2°. It travels at approximately 11,057 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 PALAPA B4 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 B4 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 13.2°, 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 B4’s average altitude, there are currently 62 active payloads and 29 tracked debris or rocket body fragments. Indonesia operates approximately 17 active satellites in total, of which 2 share a similar altitude band with PALAPA B4.
❓ Frequently Asked Questions
PALAPA B4 orbits at approximately 35,880 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 11,057 km/h — it just keeps pace with the ground below. With an inclination of 13.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
PALAPA B4 is operated by Indonesia. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21964. You can track PALAPA B4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PALAPA B4 was launched on 1992-05-14 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 PALAPA B4 (NORAD ID 21964) 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 B4 travels at approximately 11,057 km/h (6,871 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.