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Home Library Satellite Directory ASC 1 R/B(PAM-D)

ASC 1 R/B(PAM-D)

NORAD 16007 Rocket Body MEO 1985-076G
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
417 km
Apogee
34216 km
Inclination
26.5°
Period
605.0 min
Mean Motion
2.38028281 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,317 km
Orbital Velocity14,768 km/h
Velocity4.10 km/s
Orbital Period10 hours 5 minutes
Orbits / Day2.38
Eccentricity0.7134
Semi-Major Axis23,688 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1985-08-27
Launch Site
Cape Canaveral, Florida
Int'l Designator
1985-076G
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ASC 1 R/B(PAM-D) is a spent rocket body associated with United States, launched on 1985-08-27 from Cape Canaveral, Florida on the OV-103 PAM deploy/Rend 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 417 km and 34,216 km with an inclination of 26.5°. It travels at approximately 14,768 km/h (4.10 km/s), completing one full orbit every 10 hours 5 minutes — that’s roughly 2.38 orbits per day. Its orbital eccentricity of 0.7134 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like ASC 1 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
ASC 1 R/B(PAM-D) orbits at an average altitude of 17,317 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 ASC 1 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 26.5°, ASC 1 R/B(PAM-D) passes over latitudes between 26.5°N and 26.5°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
ASC 1 R/B(PAM-D) orbits in Medium Earth Orbit (MEO) at altitudes between 417 km (perigee) and 34,216 km (apogee), with an average altitude of approximately 17,317 km. It completes one orbit every 10 hours 5 minutes, travelling at approximately 14,768 km/h (9,176 mph).
ASC 1 R/B(PAM-D) (NORAD ID 16007) 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.
ASC 1 R/B(PAM-D) was launched on 1985-08-27 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 ASC 1 R/B(PAM-D) (NORAD ID 16007) 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.
ASC 1 R/B(PAM-D) travels at approximately 14,768 km/h (9,176 mph) — roughly 4.10 km/s. It completes 2.38 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.