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LES 2 AKM

NORAD 2529 Rocket Body MEO 1965-034D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
2773 km
Apogee
14802 km
Inclination
32.2°
Period
309.8 min
Mean Motion
4.64839200 rev/day
TLE Epoch
2026-09-11 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude8,788 km
Orbital Velocity18,460 km/h
Velocity5.13 km/s
Orbital Period5 hours 10 minutes
Orbits / Day4.65
Eccentricity0.3968
Semi-Major Axis15,159 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-05-06
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1965-034D
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LES 2 AKM is a spent rocket body associated with United States, launched on 1965-05-06 from Cape Canaveral Space Force Station, United States on the LES 2 launch. After more than 61 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 2,773 km and 14,802 km with an inclination of 32.2°. It travels at approximately 18,460 km/h (5.13 km/s), completing one full orbit every 5 hours 10 minutes — that’s roughly 4.65 orbits per day. Its orbital eccentricity of 0.3968 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like LES 2 AKM 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
LES 2 AKM orbits at an average altitude of 8,788 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 LES 2 AKM’s average altitude, there are currently 2 active payloads and 8 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 32.2°, LES 2 AKM passes over latitudes between 32.2°N and 32.2°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
LES 2 AKM orbits in Medium Earth Orbit (MEO) at altitudes between 2,773 km (perigee) and 14,802 km (apogee), with an average altitude of approximately 8,788 km. It completes one orbit every 5 hours 10 minutes, travelling at approximately 18,460 km/h (11,471 mph).
LES 2 AKM (NORAD ID 2529) 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.
LES 2 AKM was launched on 1965-05-06 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 LES 2 AKM (NORAD ID 2529) 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.
LES 2 AKM travels at approximately 18,460 km/h (11,471 mph) — roughly 5.13 km/s. It completes 4.65 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 sunrises and sunsets every 24 hours.