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 23083.43947265 .01653496 16475-2 32871-2 0 9990
2 40900 97.3454 112.9663 0004775 166.9063 303.7301 16.00294824417958
| Epoch (UTC): | 24 March 2023 10:32:50 |
| Eccentricity: | 0.0004775 |
| inclination: | 97.3454° |
| perigee height: | 270 km |
| apogee height: | 277 km |
| right ascension of ascending node: | 112.9663° |
| argument of perigee: | 166.9063° |
| revolutions per day: | 16.00294824 |
| mean anomaly at epoch: | 303.7301° |
| orbit number at epoch: | 41795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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