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NASA CCSDS 502.0-B : ISSUE 2 COR 1 2012

Current

Current

The latest, up-to-date edition.

ORBIT DATA MESSAGES

Published date

25-02-2014

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1 INTRODUCTION
2 OVERVIEW
3 ORBIT PARAMETER MESSAGE (OPM)
4 ORBIT MEAN-ELEMENTS MESSAGE (OMM)
5 ORBIT EPHEMERIS MESSAGE (OEM)
6 ORBIT DATA MESSAGE SYNTAX
7 SECURITY
ANNEX A - VALUES FOR TIME_SYSTEM AND FRAME RELATED
          KEYWORDS (normative)
ANNEX B - ABBREVIATIONS AND ACRONYMS (informative)
ANNEX C - RATIONALE FOR ORBIT DATA MESSAGES (informative)
ANNEX D - ITEMS FOR AN INTERFACE CONTROL DOCUMENT
          (informative)
ANNEX E - CHANGES IN ODM VERSION 2 (informative)
ANNEX F - CREATING A VERSION 1.0 COMPLIANT OPM/OEM
          (informative)
ANNEX G - INFORMATIVE REFERENCES (informative)

Defines three standard message formats for use in transferring spacecraft orbit information between space agencies and commercial or governmental spacecraft operators: the Orbit Parameter Message (OPM), the Orbit Mean-Elements Message (OMM), and the Orbit Ephemeris Message (OEM). Such exchanges are used for: a) pre-flight planning for tracking or navigation support; b) scheduling tracking support; c) carrying out tracking operations (sometimes called metric predicts); d) performing orbit comparisons; e) carrying out navigation operations such as orbit propagation and orbit reconstruction; f) assessing mutual physical and electromagnetic interference among satellites orbiting the same celestial body (currently primarily Earth, Moon, and Mars); g) performing orbit conjunction (collision avoidance) studies; and h) developing and executing collaborative maneuvers to mitigate interference or enhance mutual operations.

DocumentType
Standard
PublisherName
National Aeronautics and Space Administration
Status
Current
Supersedes

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