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 00011U 59001A 23030.48547463 .00001734 00000-0 90842-3 0 9997
2 00011 32.8795 60.8527 1463595 256.3493 87.0395 11.86434308388628
Epoch (UTC): | 30 January 2023 11:39:05 |
Eccentricity: | 0.1463595 |
inclination: | 32.8795° |
perigee height: | 553 km |
apogee height: | 2930 km |
right ascension of ascending node: | 60.8527° |
argument of perigee: | 256.3493° |
revolutions per day: | 11.86434308 |
mean anomaly at epoch: | 87.0395° |
orbit number at epoch: | 38862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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