VEP

VEP is an active satellite operated by Japan, launched on 1994-02-03 from TNSTA. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 439 km and 35,862 km with an inclination of 29.1°. It travels at approximately 14,514 km/h (4.03 km/s), completing one full orbit every 10 hours 37 minutes — that’s roughly 2.26 orbits per day. Its orbital eccentricity of 0.7223 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Geo Protected Plus constellation group. Orbital Radar tracks VEP in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.

VEP operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.