Accession Number:

AD0720823

Title:

Orbit Averaged Variation of Earth Satellite Orbital Elements

Descriptive Note:

Technical note

Corporate Author:

MASSACHUSETTS INST OF TECH LEXINGTON LINCOLN LAB

Personal Author(s):

Report Date:

1971-02-22

Pagination or Media Count:

38.0

Abstract:

An orbit averaging numerical integration method for determining the variation in the shape and orientation of an earth satellite orbit is discussed.

Subject Categories:

  • Spacecraft Trajectories and Reentry

Distribution Statement:

APPROVED FOR PUBLIC RELEASE