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 40302U 14070E 23083.66671326 .00022212 00000-0 82604-3 0 9996
2 40302 97.1294 99.7198 0029190 306.0534 163.9586 15.27117587464060
| Epoch (UTC): | 24 March 2023 16:00:04 |
| Eccentricity: | 0.0029190 |
| inclination: | 97.1294° |
| perigee height: | 464 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 99.7198° |
| argument of perigee: | 306.0534° |
| revolutions per day: | 15.27117587 |
| mean anomaly at epoch: | 163.9586° |
| orbit number at epoch: | 46406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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