ANIK C3 R/B(PAM-D)
NORAD 13666
Rocket Body
MEO
1982-110E
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
353 km
Apogee
32449 km
Inclination
23.3°
Period
570.3 min
Mean Motion
2.52522694 rev/day
TLE Epoch
2026-06-26 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude16,401 km
Orbital Velocity15,062 km/h
Velocity4.18 km/s
Orbital Period9 hours 30 minutes
Orbits / Day2.53
Eccentricity0.7047
Semi-Major Axis22,772 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1982-11-11
Launch Site
Cape Canaveral, Florida
Int'l Designator
1982-110E
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ANIK C3 R/B(PAM-D) is a spent rocket body associated with United States, launched on 1982-11-11 from Cape Canaveral, Florida on the OV-102 PAM deploy launch. With over 44 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 353 km and 32,449 km with an inclination of 23.3°. It travels at approximately 15,062 km/h (4.18 km/s), completing one full orbit every 9 hours 30 minutes — that’s roughly 2.53 orbits per day. Its orbital eccentricity of 0.7047 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like ANIK C3 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
ANIK C3 R/B(PAM-D) orbits at an average altitude of 16,401 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. With an inclination of 23.3°, ANIK C3 R/B(PAM-D) passes over latitudes between 23.3°N and 23.3°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
ANIK C3 R/B(PAM-D) orbits in Medium Earth Orbit (MEO) at altitudes between 353 km (perigee) and 32,449 km (apogee), with an average altitude of approximately 16,401 km. It completes one orbit every 9 hours 30 minutes, travelling at approximately 15,062 km/h (9,359 mph).
ANIK C3 R/B(PAM-D) (NORAD ID 13666) 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.
ANIK C3 R/B(PAM-D) was launched on 1982-11-11 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 ANIK C3 R/B(PAM-D) (NORAD ID 13666) 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.
ANIK C3 R/B(PAM-D) travels at approximately 15,062 km/h (9,359 mph) — roughly 4.18 km/s. It completes 2.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.