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 23080.31077460 .00000130 00000-0 79384-4 0 9994
2 40069 98.4269 90.3567 0004785 229.5052 130.5710 14.20757571451172
Epoch (UTC): | 21 March 2023 07:27:30 |
Eccentricity: | 0.0004785 |
inclination: | 98.4269° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 90.3567° |
argument of perigee: | 229.5052° |
revolutions per day: | 14.20757571 |
mean anomaly at epoch: | 130.5710° |
orbit number at epoch: | 45117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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