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 27833U 03028D 23088.50794829 .00000082 00000-0 51670-2 0 9992
2 27833 6.4483 199.7322 7150271 158.8028 260.1586 2.26216206163452
Epoch (UTC): | 29 March 2023 12:11:26 |
Eccentricity: | 0.7150271 |
inclination: | 6.4483° |
perigee height: | 607 km |
apogee height: | 35661 km |
right ascension of ascending node: | 199.7322° |
argument of perigee: | 158.8028° |
revolutions per day: | 2.26216206 |
mean anomaly at epoch: | 260.1586° |
orbit number at epoch: | 16345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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