ARABSAT 1B R/B(PAM-D)
NORAD 15836
Rocket Body
MEO
1985-048G
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🛰️ Orbital Parameters
Perigee
381 km
Apogee
33642 km
Inclination
27.1°
Period
593.3 min
Mean Motion
2.42700898 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,012 km
Orbital Velocity14,864 km/h
Velocity4.13 km/s
Orbital Period9 hours 53 minutes
Orbits / Day2.43
Eccentricity0.7112
Semi-Major Axis23,383 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 Arabsat (United States)
Launch Date
1985-06-17
Launch Site
Cape Canaveral, Florida
Int'l Designator
1985-048G
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ARABSAT 1B R/B(PAM-D) is a spent rocket body associated with United States, launched on 1985-06-17 from Cape Canaveral, Florida on the OV-103 PAM deploy/FF launch. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 381 km and 33,642 km with an inclination of 27.1°. It travels at approximately 14,864 km/h (4.13 km/s), completing one full orbit every 9 hours 53 minutes — that’s roughly 2.43 orbits per day. Its orbital eccentricity of 0.7112 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like ARABSAT 1B 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
ARABSAT 1B R/B(PAM-D) orbits at an average altitude of 17,012 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 ARABSAT 1B R/B(PAM-D)’s average altitude, there are currently 0 active payloads and 8 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 27.1°, ARABSAT 1B R/B(PAM-D) passes over latitudes between 27.1°N and 27.1°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 12,413 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
ARABSAT 1B R/B(PAM-D) orbits in Medium Earth Orbit (MEO) at altitudes between 381 km (perigee) and 33,642 km (apogee), with an average altitude of approximately 17,012 km. It completes one orbit every 9 hours 53 minutes, travelling at approximately 14,864 km/h (9,236 mph).
ARABSAT 1B R/B(PAM-D) (NORAD ID 15836) 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.
ARABSAT 1B R/B(PAM-D) was launched on 1985-06-17 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. 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 ARABSAT 1B R/B(PAM-D) (NORAD ID 15836) 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.
ARABSAT 1B R/B(PAM-D) travels at approximately 14,864 km/h (9,236 mph) — roughly 4.13 km/s. It completes 2.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.