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SOLRAD 11A/B PKM

NORAD 8752 Rocket Body MEO 1976-023G
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36238 km
Apogee
102751 km
Inclination
21.7°
Period
3466.5 min
Mean Motion
0.41540803 rev/day
TLE Epoch
2026-09-07 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude69,495 km
Orbital Velocity8,252 km/h
Velocity2.29 km/s
Orbital Period57.8 hours
Orbits / Day0.42
Eccentricity0.4384
Semi-Major Axis75,866 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1976-03-15
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1976-023G
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SOLRAD 11A/B PKM is a spent rocket body associated with United States, launched on 1976-03-15 from Cape Canaveral Space Force Station, United States on the LES 8 launch. After more than 50 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 36,238 km and 102,751 km with an inclination of 21.7°. It travels at approximately 8,252 km/h (2.29 km/s), completing one full orbit every 57.8 hours — that’s roughly 0.42 orbits per day. Its orbital eccentricity of 0.4384 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like SOLRAD 11A/B PKM 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
SOLRAD 11A/B PKM orbits at an average altitude of 69,495 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 21.7°, SOLRAD 11A/B PKM passes over latitudes between 21.7°N and 21.7°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 13,206 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
SOLRAD 11A/B PKM orbits in Medium Earth Orbit (MEO) at altitudes between 36,238 km (perigee) and 102,751 km (apogee), with an average altitude of approximately 69,495 km. It completes one orbit every 57.8 hours, travelling at approximately 8,252 km/h (5,127 mph).
SOLRAD 11A/B PKM (NORAD ID 8752) 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.
SOLRAD 11A/B PKM was launched on 1976-03-15 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. View the full satellite launch log.
Yes — Orbital Radar tracks SOLRAD 11A/B PKM (NORAD ID 8752) 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.
SOLRAD 11A/B PKM travels at approximately 8,252 km/h (5,127 mph) — roughly 2.29 km/s. It completes 0.42 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 1 sunrises and sunsets every 24 hours.