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 23090.80409412 .00000102 00000-0 66536-4 0 9999
2 40069 98.4259 100.3649 0005204 195.7718 164.3290 14.20760793452667
Epoch (UTC): | 31 March 2023 19:17:53 |
Eccentricity: | 0.0005204 |
inclination: | 98.4259° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 100.3649° |
argument of perigee: | 195.7718° |
revolutions per day: | 14.20760793 |
mean anomaly at epoch: | 164.3290° |
orbit number at epoch: | 45266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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