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 40071U 14037C 23079.25349553 .00002743 00000-0 34750-3 0 9992
2 40071 98.3725 326.1950 0009012 143.6314 216.5503 14.82634677470199
Epoch (UTC): | 20 March 2023 06:05:02 |
Eccentricity: | 0.0009012 |
inclination: | 98.3725° |
perigee height: | 615 km |
apogee height: | 627 km |
right ascension of ascending node: | 326.1950° |
argument of perigee: | 143.6314° |
revolutions per day: | 14.82634677 |
mean anomaly at epoch: | 216.5503° |
orbit number at epoch: | 47019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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