PALAPA B1 R/B(PAM-D)
NORAD 14136
Rocket Body
MEO
1983-059E
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🛰️ Orbital Parameters
Perigee
306 km
Apogee
30349 km
Inclination
25.8°
Period
530.4 min
Mean Motion
2.71492366 rev/day
TLE Epoch
2026-10-15 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude15,328 km
Orbital Velocity15,430 km/h
Velocity4.29 km/s
Orbital Period8 hours 50 minutes
Orbits / Day2.71
Eccentricity0.6923
Semi-Major Axis21,699 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-06-18
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1983-059E
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
PALAPA B1 R/B(PAM-D) is a spent rocket body associated with United States, launched on 1983-06-18 from Cape Canaveral Space Force Station, United States on the OV-099 PAM deploy/FF launch. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 306 km and 30,349 km with an inclination of 25.8°. It travels at approximately 15,430 km/h (4.29 km/s), completing one full orbit every 8 hours 50 minutes — that’s roughly 2.71 orbits per day. Its orbital eccentricity of 0.6923 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like PALAPA B1 R/B(PAM-D) are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
PALAPA B1 R/B(PAM-D) orbits at an average altitude of 15,328 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of PALAPA B1 R/B(PAM-D)’s average altitude, there are currently 0 active payloads and 6 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 25.8°, PALAPA B1 R/B(PAM-D) passes over latitudes between 25.8°N and 25.8°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 13,201 active satellites in total.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
PALAPA B1 R/B(PAM-D) orbits in Medium Earth Orbit (MEO) at altitudes between 306 km (perigee) and 30,349 km (apogee), with an average altitude of approximately 15,328 km. It completes one orbit every 8 hours 50 minutes, travelling at approximately 15,430 km/h (9,588 mph).
PALAPA B1 R/B(PAM-D) (NORAD ID 14136) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
PALAPA B1 R/B(PAM-D) was launched on 1983-06-18 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks PALAPA B1 R/B(PAM-D) (NORAD ID 14136) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 B1 R/B(PAM-D) travels at approximately 15,430 km/h (9,588 mph) — roughly 4.29 km/s. It completes 2.71 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.