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 40908U 15049K 23160.84886934 .00005157 00000-0 24469-3 0 9998
2 40908 97.5247 163.9269 0013076 208.7112 151.3404 15.19643068426688
| Epoch (UTC): | 09 June 2023 20:22:22 |
| Eccentricity: | 0.0013076 |
| inclination: | 97.5247° |
| perigee height: | 498 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 163.9269° |
| argument of perigee: | 208.7112° |
| revolutions per day: | 15.19643068 |
| mean anomaly at epoch: | 151.3404° |
| orbit number at epoch: | 42668 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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