# data[].attributes.body
weather
earth surface changes
agriculture

# data[].attributes.body
Lunar
ISS
weather
imagery
GPS

# data[].attributes.body
apogee is over Russia for a long period of time
Communications for long hang time over Russia
not good for imagery as too far away, when at perigee going too fast for imagery

# data[].attributes.body
navigation
communication
geo/space environment science

# data[].attributes.body
90 mins roughly
18 revolutions roughly

# data[].attributes.body
large apogee - slow here
very fast at perigee

# data[].attributes.body
No minimum
approximately 350 km is the ISS

# data[].attributes.body
2,000 km roughly
lower than 35,000 km
higher than 2,000 km
most common- 20,200 km

# data[].attributes.body
12 hrs roughly
no more than 23.5

# data[].attributes.body
Galileo
Glonass
Telstar 1

# data[].attributes.body
over 35,786 km

# data[].attributes.body
longer than24 hours
Earth is rotating faster than the satellite orbit period so ground trace appears to go west ward

# data[].attributes.body
stays in one spot with respect of the earth
36,000 km
0º inclination
geostationary belt- belt like appearance around the earth, limited resources.

# data[].attributes.body
Exactly 24 hours

# data[].attributes.body
High inclination
highly elliptical-large semi-major axis, high eccentricity

# data[].attributes.body
Passes over the same part of earth at the same time every day

# data[].attributes.body
varies
must have 90º inclination

# data[].attributes.body
Group that preforms a mission together
do not have to be in the same orbit type