REFINEMENT OF ALOUETTE 1 ORBIT, FOR THE PERIOD 27 APRIL-6 MAY 1964.

Abstract

The orbit of Alouette 1 was computed by N.A.S.A. from observations made by Minitrack stations. For the ten-day period 27 April-6 May 1964, this orbit is refined using the same observations, by Merson's differential correction method. A comparison between the refined and N.A.S.A. orbits shows good agreement for semi major axis and right ascension of the ascending node. However, significant discrepancies occur for eccentricity and argument of perigee.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
AD0482737

Entities

People

  • H. Hiller

Organizations

  • Royal Aircraft Establishment

Tags

DTIC Thesaurus Topics

  • Acquisition
  • Agreements
  • Eccentricity
  • Observation

Readers

  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Space
  • Space - Orbital Debris