Informējam, ka Sistēma pielāgota darbam ar interneta pārlūkprogrammu Internet Explorer (8. un jaunākām versijām) un Mozilla Firefox (3.6 un jaunākām versijām).
Izmantojot citu interneta pārlūkprogrammu, brīdinām, ka Sistēmas funkcionalitāte var tikt traucēta.
<p>ISO 26900:2012 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</p>
<p>a) pre-flight planning for tracking or navigation support,</p>
<p>b) scheduling tracking support,</p>
<p>c) carrying out tracking operations (sometimes called metric predicts),</p>
<p>d) performing orbit comparisons,</p>
<p>e) carrying out navigation operations such as orbit propagation and orbit reconstruction,</p>
<p>f) assessing mutual physical and electromagnetic interference among satellites orbiting the same celestial body (currently primarily Earth, Moon, and Mars),</p>
<p>g) performing orbit conjunction (collision avoidance) studies, and </p>
<p>h) developing and executing collaborative manoeuvres to mitigate interference or enhance mutual operations. </p>
<p>ISO 26900:2012 includes sets of requirements and criteria that the message formats have been designed to meet.</p>
Reģistrācijas numurs (WIID)
46135
Darbības sfēra
<p>ISO 26900:2012 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</p>
<p>a) pre-flight planning for tracking or navigation support,</p>
<p>b) scheduling tracking support,</p>
<p>c) carrying out tracking operations (sometimes called metric predicts),</p>
<p>d) performing orbit comparisons,</p>
<p>e) carrying out navigation operations such as orbit propagation and orbit reconstruction,</p>
<p>f) assessing mutual physical and electromagnetic interference among satellites orbiting the same celestial body (currently primarily Earth, Moon, and Mars),</p>
<p>g) performing orbit conjunction (collision avoidance) studies, and </p>
<p>h) developing and executing collaborative manoeuvres to mitigate interference or enhance mutual operations. </p>
<p>ISO 26900:2012 includes sets of requirements and criteria that the message formats have been designed to meet.</p>
