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 37841U 11058D 23089.09713963 .00000598 00000-0 18344-3 0 9993
2 37841 19.9732 328.1983 0011829 242.3975 271.7293 14.10862586591842
Epoch (UTC): | 30 March 2023 02:19:52 |
Eccentricity: | 0.0011829 |
inclination: | 19.9732° |
perigee height: | 848 km |
apogee height: | 865 km |
right ascension of ascending node: | 328.1983° |
argument of perigee: | 242.3975° |
revolutions per day: | 14.10862586 |
mean anomaly at epoch: | 271.7293° |
orbit number at epoch: | 59184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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