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 40910U 15049M 23087.97219120 .00039567 00000-0 12440-2 0 9997
2 40910 97.4684 100.0618 0012444 60.4434 7.4065 15.32790813416581
| Epoch (UTC): | 28 March 2023 23:19:57 |
| Eccentricity: | 0.0012444 |
| inclination: | 97.4684° |
| perigee height: | 459 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 100.0618° |
| argument of perigee: | 60.4434° |
| revolutions per day: | 15.32790813 |
| mean anomaly at epoch: | 7.4065° |
| orbit number at epoch: | 41658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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