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BS ISO 26900:2012

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Space data and information transfer systems. Orbit data messages
Available format(s)

Hardcopy , PDF

Superseded date

15-02-2024

Language(s)

English

Published date

30-09-2015

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
          REFERENCE_FRAME (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)

Describes 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).

This International Standard specifies 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 pre-flight planning for tracking or navigation support, scheduling tracking support, carrying out tracking operations (sometimes called metric predicts), performing orbit comparisons, carrying out navigation operations such as orbit propagation and orbit reconstruction, assessing mutual physical and electromagnetic interference among satellites orbiting the same celestial body (currently primarily Earth, Moon, and Mars), performing orbit conjunction (collision avoidance) studies, and developing and executing collaborative manoeuvres to mitigate interference or enhance mutual operations. This International Standard includes sets of requirements and criteria that the message formats have been designed to meet. NOTE For exchanges where these requirements do not capture the needs of the participating agencies and satellite operators, another mechanism can be selected. The scope and field of application are furthermore detailed in subclauses 1.1 and 1.2 of the enclosed CCSDS publication.

Committee
ACE/68
DevelopmentNote
Supersedes 10/30197731 DC. (10/2012)
DocumentType
Standard
Pages
86
PublisherName
British Standards Institution
Status
Superseded
SupersededBy
Supersedes

Standards Relationship
ISO 26900:2012 Identical

ISO/IEC 8859-1:1998 Information technology 8-bit single-byte coded graphic character sets Part 1: Latin alphabet No. 1
ISO 13541:2010 Space data and information transfer systems Attitude data messages
IEEE 754-2008 REDLINE IEEE Standard for Floating-Point Arithmetic
ISO 11104:2011 Space data and information transfer systems — Time code formats

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