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 40069U 14037A 23080.87417499 .00000122 00000-0 75586-4 0 9996
2 40069 98.4267 90.8940 0004781 227.6277 132.4490 14.20757658451255
Epoch (UTC): | 21 March 2023 20:58:48 |
Eccentricity: | 0.0004781 |
inclination: | 98.4267° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 90.8940° |
argument of perigee: | 227.6277° |
revolutions per day: | 14.20757658 |
mean anomaly at epoch: | 132.4490° |
orbit number at epoch: | 45125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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