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 40101U 14043C 23088.21699736 -.00000147 00000-0 00000-0 0 9995
2 40101 6.4370 67.7542 0014372 304.1032 262.8162 0.98727244 13698
| Epoch (UTC): | 29 March 2023 05:12:28 |
| Eccentricity: | 0.0014372 |
| inclination: | 6.4370° |
| perigee height: | 36163 km |
| apogee height: | 36286 km |
| right ascension of ascending node: | 67.7542° |
| argument of perigee: | 304.1032° |
| revolutions per day: | 0.98727244 |
| mean anomaly at epoch: | 262.8162° |
| orbit number at epoch: | 1369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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