altitude 705 km (nominal) · satellite orbit orbit period 98.9 minutes time of day 10:30 am (local)...

Altitude 705 km (Nominal) Ground Track Equator Inclination 98.2° Orbit Period 98.9 minutes Satellite Orbit Time of Day 10:30 am (Local) Example of a sun-synchronous polar orbit with an orbital altitude of 705 km above the Earth’s surface, an orbital period of 98.9 minutes, resulting in 14.3 orbits per day, and an orbital inclination of 98.2° at the Equator. Sun-synchronous orbits are specified in terms of the time of day they cross the equator on the sunlit side of the orbit (10:30 am local time in this Terra example).

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Altitude 705 km (Nominal)

Ground Track

EquatorInclination 98.2°

Orbit Period 98.9 minutesSatellite Orbit

Time of Day 10:30 am (Local)

Example of a sun-synchronous polarorbit with an orbital altitude of 705 kmabove the Earth’s surface, an orbital peri-od of 98.9 minutes, resulting in 14.3orbits per day, and an orbital inclinationof 98.2° at the Equator. Sun-synchronousorbits are specified in terms of the time ofday they cross the equator on the sunlitside of the orbit (10:30 am local time inthis Terra example).

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