General Orbits

Orbits are complicated, because they involve both position and velocity in three spatial dimensions and time. Simple two-body "Kepler" orbits relate the position and velocity at one time to the position and velocity at other times. In reality, orbits are also complicated by drag, light pressure, and gravitational perturbations by other bodies, and in the extreme by relativistic effects. For this discussion, we will not consider the complications, so that we get closed-form algebraic solutions. Of course, in real life, we will need to include all the complications in our calculations of orbital properties.

Server-sats are deployed in closely packed orbital families. One central orbit, perfectly circular and in the orbital plane, with a sidereal period of 14393 seconds and a radius of 12789 kilometers, surrounded by slightly inclined and slightly elliptical orbits that fill a toroidal region around that central orbit. By carefully assigning orbital parameters, this region can be filled with densely packed orbits and objects in them.

Describing Earth Orbits

Orbits are ellipses in a plane which also contains the center of the mass that defines the orbit.

MORE LATER

Well Known Earth Orbits

system

status

number

planes

#/plane

perigee

apogee

inclination

period

uplink GHz

downlink GHz

Space Station

in use

1

1

1

6727

6736

51.6

5480

x

x

Iridium

in use

66

6

11

7158

7158

86.4

6027

Ka band

Ka band

Teledesic

bankrupt

288

12

24

7778

7778

98.2

6827

28.6-29.2

18.9-19.3

Globalstar

in use

48

x

x

7792

7792

52

6845

x

x

Molniya

in use

3?

3?

1

7885

45683

63.4

43082

x

x

GPS

in use

31

6?

x

26600

26600

55

43082

x

x

GEO

in use

x

1

x

42164

42164

0

86164

x

x

Moon

natural

1

1

1

364397

406731

5.14

2360592

x

x

MORE LATER

References

SaVi satellite constellation visualization

Notes on GPS satellite orbits

Encyclopedia Astronautica

Wikipedia : Orbit

Wikipedia : Orbital Elements

MORE LATER