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 23080.26581945 .00002579 00000-0 32718-3 0 9997
2 40071 98.3726 327.2545 0008960 140.3073 219.8770 14.82638579470343
Epoch (UTC): | 21 March 2023 06:22:46 |
Eccentricity: | 0.0008960 |
inclination: | 98.3726° |
perigee height: | 615 km |
apogee height: | 627 km |
right ascension of ascending node: | 327.2545° |
argument of perigee: | 140.3073° |
revolutions per day: | 14.82638579 |
mean anomaly at epoch: | 219.8770° |
orbit number at epoch: | 47034 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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