Analysis of the Orbit of Cosmos 268 Rocket (1969-20B)

Abstract

The orbit of Cosmos 268 rocket (1969-20B) has been determined at 28 epochs during its 342-day life, with the aid of the PROP5 orbit refinement program. All available observations were used, including 16 from the Hewitt camera at Malvern, 28 from the 200-mm camera at Meudon, 56 from the kinetheodolite at the Cape Observatory, 700 visual observations from volunteer observers, 500 US Navy observations and 200 British radar observations. The orbits are of very good accuracy for such a high-drag satellite, most of the values of inclination having standard deviations less than 0.002 degree. The most accurate orbits are those utilizing photographic observations, and the best of these has standard deviations of 0.00001 in eccentricity and 0.0001 degree in inclination.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0740634

Entities

People

  • A. N. Winterbottom
  • Desmond King-Hele

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Accuracy
  • Artificial Satellites
  • Atmospheres
  • Coefficients
  • Computer Programs
  • Computers
  • Eccentricity
  • Magnetic Disturbances
  • Magnetic Storms
  • Measurement
  • Observation
  • Observatories
  • Regions
  • Satellite Orbits
  • Space Sciences
  • Stations
  • Wind

Fields of Study

  • Physics

Readers

  • Astronomy and Astrophysics.
  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Space
  • Space - Orbital Debris
  • Space - Space Objects