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 40025U 14033R 23342.43005886 .00004342 00000-0 38935-3 0 9994
2 40025 98.0190 292.7448 0013014 77.5586 282.7090 14.96254511514177
Epoch (UTC): | 08 December 2023 10:19:17 |
Eccentricity: | 0.0013014 |
inclination: | 98.0190° |
perigee height: | 569 km |
apogee height: | 587 km |
right ascension of ascending node: | 292.7448° |
argument of perigee: | 77.5586° |
revolutions per day: | 14.96254511 |
mean anomaly at epoch: | 282.7090° |
orbit number at epoch: | 51417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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