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POLAR

NORAD 23802 Payload HEO 1996-013A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
6487 km
Apogee
51738 km
Inclination
79.8°
Period
1109.0 min
Mean Motion
1.29845787 rev/day
TLE Epoch
2026-03-16 14:00:00 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
Eccentricity0.6376
Semi-Major Axis35,484 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1996-02-24
Launch Site
Vandenberg SFB, California
Int'l Designator
1996-013A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
geo protected plus
📖 About This Object
POLAR is an active satellite operated by United States, launched on 1996-02-24 from Vandenberg SFB, California. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 6,487 km and 51,738 km with an inclination of 79.8°. 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 0.6376 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 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 (HEO), which sweeps between a low-altitude perigee and a very high apogee. HEO satellites spend most of their orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest. This makes HEO ideal for high-latitude communications (Molniya and Tundra orbits), early-warning missile detection (SBIRS), and space science missions that need to sample different regions of the magnetosphere. The large difference between perigee (6,487 km) and apogee (51,738 km) for this object illustrates the characteristic elliptical shape.
❓ Frequently Asked Questions
POLAR follows a Highly Elliptical Orbit, swinging between 6,487 km (perigee) and 51,738 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 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.
POLAR was launched on 1996-02-24 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California.
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.
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.
POLAR is a member of the Geo Protected Plus constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geo Protected Plus satellites on Orbital Radar’s live tracker.