Use the gibbs method to calculate the state vector of the


A tracking station at latitude -200 and elevation 500 m makes the following observations of a satellite at the given times.

Time (min)

Local Sidereal Time (0)

Azimuth (0)

Elevation  Angle (0)

Range (km)

0

60.0

165.931

9.53549

1214.89

2

60.5014

145.967

45.7711

421.441

4

61.0027

2.40962

21.8825

732.079

Use the Gibbs method to calculate the state vector of the satellite at the central observation time.

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Microeconomics: Use the gibbs method to calculate the state vector of the
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