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 40900U 15049B 23080.22510355 .00886152 33650-3 26417-2 0 9990
2 40900 97.3566 109.4421 0003061 191.5874 183.9585 15.92459073417441
Epoch (UTC): | 21 March 2023 05:24:08 |
Eccentricity: | 0.0003061 |
inclination: | 97.3566° |
perigee height: | 293 km |
apogee height: | 297 km |
right ascension of ascending node: | 109.4421° |
argument of perigee: | 191.5874° |
revolutions per day: | 15.92459073 |
mean anomaly at epoch: | 183.9585° |
orbit number at epoch: | 41744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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