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INSAT 1B R/B(PAM-D)

NORAD 14524 Rocket Body MEO 1983-089C
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🛰️ Orbital Parameters
Perigee
302 km
Apogee
19319 km
Inclination
24.4°
Period
341.6 min
Mean Motion
4.21497818 rev/day
TLE Epoch
2026-10-15 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,811 km
Orbital Velocity17,867 km/h
Velocity4.96 km/s
Orbital Period5 hours 42 minutes
Orbits / Day4.21
Eccentricity0.5876
Semi-Major Axis16,182 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-08-30
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1983-089C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
INSAT 1B R/B(PAM-D) is a spent rocket body associated with United States, launched on 1983-08-30 from Cape Canaveral Space Force Station, United States on the OV-099 PAM deploy 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 302 km and 19,319 km with an inclination of 24.4°. It travels at approximately 17,867 km/h (4.96 km/s), completing one full orbit every 5 hours 42 minutes — that’s roughly 4.21 orbits per day. Its orbital eccentricity of 0.5876 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like INSAT 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
INSAT 1B R/B(PAM-D) orbits at an average altitude of 9,811 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 INSAT 1B R/B(PAM-D)’s average altitude, there are currently 0 active payloads and 11 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 24.4°, INSAT 1B R/B(PAM-D) passes over latitudes between 24.4°N and 24.4°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
INSAT 1B R/B(PAM-D) orbits in Medium Earth Orbit (MEO) at altitudes between 302 km (perigee) and 19,319 km (apogee), with an average altitude of approximately 9,811 km. It completes one orbit every 5 hours 42 minutes, travelling at approximately 17,867 km/h (11,102 mph).
INSAT 1B R/B(PAM-D) (NORAD ID 14524) 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.
INSAT 1B R/B(PAM-D) was launched on 1983-08-30 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 INSAT 1B R/B(PAM-D) (NORAD ID 14524) 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.
INSAT 1B R/B(PAM-D) travels at approximately 17,867 km/h (11,102 mph) — roughly 4.96 km/s. It completes 4.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 sunrises and sunsets every 24 hours.