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 23090.52381078 .00002618 00000-0 33149-3 0 9995
2 40071 98.3704 337.9883 0009359 111.2756 248.9443 14.82694356471863
Epoch (UTC): | 31 March 2023 12:34:17 |
Eccentricity: | 0.0009359 |
inclination: | 98.3704° |
perigee height: | 614 km |
apogee height: | 627 km |
right ascension of ascending node: | 337.9883° |
argument of perigee: | 111.2756° |
revolutions per day: | 14.82694356 |
mean anomaly at epoch: | 248.9443° |
orbit number at epoch: | 47186 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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