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 23341.92944094 .00016223 00000-0 47476-3 0 9993
2 40911 97.4855 351.7528 0006779 260.1624 99.8854 15.35308599454954
| Epoch (UTC): | 07 December 2023 22:18:23 |
| Eccentricity: | 0.0006779 |
| inclination: | 97.4855° |
| perigee height: | 455 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 351.7528° |
| argument of perigee: | 260.1624° |
| revolutions per day: | 15.35308599 |
| mean anomaly at epoch: | 99.8854° |
| orbit number at epoch: | 45495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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