POLAR
NORAD 23802
Payload
HEO
1996-013A
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HEO · NORAD 23802
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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
5828 km
Apogee
52397 km
Inclination
80.0°
Period
1109.0 min
Mean Motion
1.29845742 rev/day
TLE Epoch
2026-09-16 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude29,113 km
Orbital Velocity12,066 km/h
Velocity3.35 km/s
Orbital Period18 hours 29 minutes
Orbits / Day1.30
Eccentricity0.6562
Semi-Major Axis35,484 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 GSFC (United States)
Launch Date
1996-02-24
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1996-013A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
POLAR is an active satellite operated by GSFC (United States), launched on 1996-02-24 from Vandenberg Space Force Base, United States on the Polar launch. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 5,828 km and 52,397 km with an inclination of 80.0°. It travels at approximately 12,066 km/h (3.35 km/s), completing one full orbit every 18 hours 29 minutes — that’s roughly 1.30 orbits per day. Its orbital eccentricity of 0.6562 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks POLAR in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
POLAR follows a Highly Elliptical Orbit, sweeping between 5,828 km (perigee) and 52,397 km (apogee). It spends most of its 18 hours 29 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 80.0°, POLAR passes over latitudes between 80.0°N and 80.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,204 active satellites in total.
❓ Frequently Asked Questions
POLAR follows a Highly Elliptical Orbit, swinging between 5,828 km (perigee) and 52,397 km (apogee). It spends most of its 18 hours 29 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
POLAR is operated by GSFC (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23802. You can track POLAR in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
POLAR was launched on 1996-02-24 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. View the full satellite launch log.
Yes — Orbital Radar tracks POLAR (NORAD ID 23802) 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.
POLAR’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 12,066 km/h (3.35 km/s), completing one revolution every 18 hours 29 minutes. Learn more about highly elliptical orbits.