Samos 2 (1961alpha1): orbit determination and analysis at 31:2 resonance

Samos 2 (1961alpha1): orbit determination and analysis at 31:2 resonance

Walker, D.M.C.

Royal Aircraft Establishment RAE

1980-02-28

Samos 2, 1961alpha1, launched on 31 January 1961, was the first satellite to enter a sun-synchronous orbit at an inclination of 97.4º. The initial perigee and apogee heights were 474 km and 557 km respectively, the initial period was 94.97 minutes and the satellite decayed on 21 October 1973 after more than 12 years in orbit. Samos 2 passed through the condition of 31:2 resonance in June 1971 and orbital parameters have been determined at 22 epochs from 1674 observations using the RAE orbit refinement program, PROP, between mid-April and mid-September 1971. The variations of inclination and eccentricity during this time have been analysed and values for six lumped 31st-order harmonie coefficients in the geopotential have been obtained. These lumped harmonie coefficients have been compared with those derived from the individual coefficients, of order 31 and appropriate degrees, from the most recent Goddard Earth Model, GEM IOC. The decrease in inclination between launch and 1971 has been examined: it is found to be caused mainly by a near-resonant solar gravitational perturbation.

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Procurement Executive, Ministry of Defence, Royal Aircraft Establishment, RAE Farnborough

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RAE Technical Report No. 80022

Aerospace Engineering Reports

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© 1980 Controller HMSO London