Examples of using Perigee in English and their translations into Arabic
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Colloquial
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Political
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Ecclesiastic
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Ecclesiastic
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Computer
The distribution of the 500 largest space debris objects makes it possible to identify a high collision risk by looking at the relationship between the apogee and perigee altitudes versus inclination distributions of the existing low-Earth orbit rocket bodies and spacecraft that have the highest mass and collision probability products.
The Ørsted orbit has an inclination of ~96.5°, a period of ~100 minutes, a perigee at ~650 km and an apogee at ~860 km(decreased to respectively 99.59 min, 636 km and 842 km after 11 years and 8 months in space).
Several manoeuvres were performed between 11 and 15 April 2011, followed by a venting of the fuel pipes and tanks to achieve a final orbit of approximately 350 km(perigee) x 384 km(apogee) above the geostationary ring with a final spin rate of approximately 72 rpm(with
Perigee altitude.
Kilometres Perigee.
Perigee: 717.640 kilometres.
(d) Perigee: 253.0 kilometres.
Time of perigee passage.
(d) Perigee: 35,776 kilometres.
Perigee radius: 42,164 km(geostationary).
(d) Perigee 980 km.
Well, it has a mathematically proven perigee.
(d) Perigee: 200 kilometres.
A Satellite currently being manoeuvred to lower the perigee.
Therefore their perigee and apogee altitudes have not been listed.
The satellite is in a graveyard orbit, at a perigee of 400 km above the geostationary orbit.
(deorbiting manoeuvres effected in November 2003 to lower the satellite ' s perigee to below 600 km with a view to achieving re-entry within 25 years).
(final deorbiting manoeuvres effected on 21 October 2004 to lower the satellite ' s perigee to below 600 km with a view to achieving re-entry within 25 years).
(final deorbiting manoeuvres effected on 29 July 2009 to lower the satellite ' s perigee to below 600 km with a view to achieving re-entry within 25 years).
SPOT 1 Earth observation satellite(deorbiting manoeuvres effected in November 2003 to lower the satellite ' s perigee to below 600 km with a view to achieving re-entry within 25 years).