LEASAT 1 PKM
NORAD 15390
Rocket Body
MEO
1984-113E
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
216 km
Apogee
7088 km
Inclination
27.1°
Period
166.6 min
Mean Motion
8.64465830 rev/day
TLE Epoch
2026-06-25 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,652 km
Orbital Velocity22,702 km/h
Velocity6.31 km/s
Orbital Period2 hours 47 minutes
Orbits / Day8.64
Eccentricity0.3428
Semi-Major Axis10,023 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1984-11-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1984-113E
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
LEASAT 1 PKM is a spent rocket body associated with United States, launched on 1984-11-08 from Cape Canaveral, Florida on the OV-103 PAM deploy/Rend launch. With over 42 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 216 km and 7,088 km with an inclination of 27.1°. It travels at approximately 22,702 km/h (6.31 km/s), completing one full orbit every 2 hours 47 minutes — that’s roughly 8.64 orbits per day. Its orbital eccentricity of 0.3428 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like LEASAT 1 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
LEASAT 1 PKM orbits at an average altitude of 3,652 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 LEASAT 1 PKM’s average altitude, there are currently 1 active payload and 4 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°, LEASAT 1 PKM 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
LEASAT 1 PKM orbits in Medium Earth Orbit (MEO) at altitudes between 216 km (perigee) and 7,088 km (apogee), with an average altitude of approximately 3,652 km. It completes one orbit every 2 hours 47 minutes, travelling at approximately 22,702 km/h (14,107 mph).
LEASAT 1 PKM (NORAD ID 15390) 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.
LEASAT 1 PKM was launched on 1984-11-08 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 LEASAT 1 PKM (NORAD ID 15390) 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.
LEASAT 1 PKM travels at approximately 22,702 km/h (14,107 mph) — roughly 6.31 km/s. It completes 8.64 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 17 sunrises and sunsets every 24 hours.