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 23331.91151426 .00003209 00000-0 39490-3 0 9990
2 40071 98.3430 230.2823 0009363 61.1153 299.0998 14.83708899507554
Epoch (UTC): | 27 November 2023 21:52:34 |
Eccentricity: | 0.0009363 |
inclination: | 98.3430° |
perigee height: | 611 km |
apogee height: | 624 km |
right ascension of ascending node: | 230.2823° |
argument of perigee: | 61.1153° |
revolutions per day: | 14.83708899 |
mean anomaly at epoch: | 299.0998° |
orbit number at epoch: | 50755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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