View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 29507U 06046C 21065.81423228 .00000893 00000-0 73777-4 0 9998
2 29507 97.7206 92.2822 0048812 2.7345 357.4136 15.00683508784717
Epoch (UTC): | 06 March 2021 19:32:29 |
Eccentricity: | 0.0048812 |
inclination: | 97.7206° |
perigee height: | 531 km |
apogee height: | 598 km |
right ascension of ascending node: | 92.2822° |
argument of perigee: | 2.7345° |
revolutions per day: | 15.00683508 |
mean anomaly at epoch: | 357.4136° |
orbit number at epoch: | 78471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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