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 40907U 15049J 23090.81112550 .00021126 00000-0 82464-3 0 9995
2 40907 97.4959 98.1397 0013706 71.7058 11.3168 15.25844187416676
Epoch (UTC): | 31 March 2023 19:28:01 |
Eccentricity: | 0.0013706 |
inclination: | 97.4959° |
perigee height: | 479 km |
apogee height: | 497 km |
right ascension of ascending node: | 98.1397° |
argument of perigee: | 71.7058° |
revolutions per day: | 15.25844187 |
mean anomaly at epoch: | 11.3168° |
orbit number at epoch: | 41667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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