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 39765U 14028E 23081.80621373 .00000030 00000-0 77584-4 0 9997
2 39765 82.4522 330.2427 0230424 257.5600 99.9633 12.82859007413623
Epoch (UTC): | 22 March 2023 19:20:56 |
Eccentricity: | 0.0230424 |
inclination: | 82.4522° |
perigee height: | 1152 km |
apogee height: | 1507 km |
right ascension of ascending node: | 330.2427° |
argument of perigee: | 257.5600° |
revolutions per day: | 12.82859007 |
mean anomaly at epoch: | 99.9633° |
orbit number at epoch: | 41362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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