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 23091.89182213 .00039686 00000-0 12363-2 0 9991
2 40910 97.4693 104.0227 0012096 48.7508 35.8066 15.33087422417184
| Epoch (UTC): | 01 April 2023 21:24:13 |
| Eccentricity: | 0.0012096 |
| inclination: | 97.4693° |
| perigee height: | 458 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 104.0227° |
| argument of perigee: | 48.7508° |
| revolutions per day: | 15.33087422 |
| mean anomaly at epoch: | 35.8066° |
| orbit number at epoch: | 41718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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