# data[].attributes.body
Groups that performs a mission together
Do not have to be in the same orbit type

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Varies from LEO to HEO
Must have 90 degree inclination
ground-trace will eventually cover all of Earth
Passes over the same part of Earth at the same time each day

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Weather
Earth surface changes
Agriculture

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Apogee is over Russia for a long period of time
Communication for long hang time over Russia
Not good for imagery - too far away or too fast

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Large Apogee - slow here
Perigee - fast af boiiii

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High inclination
Highly elliptical - large semi-major axis, high eccentricity

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communication
permanent relay stations

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Exactly 24 hours
ground trace inclination up to +/-70 degrees

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stays in one spot with respect the Earth
36,000 km
0 degree inclination
Geostationary belt - belt around Earth
Limited resources

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over 35,786

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Longer than 24 hours
Earth is rotating faster than the satellite orbit period so ground trace appears to go westward

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As low as possible as long as it can stay in orbit
Period of about 90 minutes
All manned space missions except lunar missions

Missions/Purposes:
Lunar Iss
GPS
weather
imagery

# data[].attributes.body
Regioni above LEO, but below geosynchronous
lower than 35000
higher than 2000
Most common is 20,200

Period of about 12 hours and no more than 23.5 hours, 18 times per day roughly

Mission/Purpose:
navigation
communication
geo/space

Famous Names
Glonass
Galileo
Telstar 1