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 40911U 15049N 23086.13628484 .00020363 00000-0 80411-3 0 9990
2 40911 97.4931 93.9392 0013784 88.4644 336.6351 15.25464055415848
| Epoch (UTC): | 27 March 2023 03:16:15 |
| Eccentricity: | 0.0013784 |
| inclination: | 97.4931° |
| perigee height: | 480 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 93.9392° |
| argument of perigee: | 88.4644° |
| revolutions per day: | 15.25464055 |
| mean anomaly at epoch: | 336.6351° |
| orbit number at epoch: | 41584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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