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 40057U 14034E 24284.04495162 .00015424 00000-0 16712-2 0 9994
2 40057 98.3248 144.8328 0009873 122.4108 237.8063 14.88276862554776
Epoch (UTC): | 10 October 2024 01:04:43 |
Eccentricity: | 0.0009873 |
inclination: | 98.3248° |
perigee height: | 596 km |
apogee height: | 610 km |
right ascension of ascending node: | 144.8328° |
argument of perigee: | 122.4108° |
revolutions per day: | 14.88276862 |
mean anomaly at epoch: | 237.8063° |
orbit number at epoch: | 55477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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