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 41465U 16026B 23340.81359523 .00054587 00000-0 41147-3 0 9992
2 41465 96.9651 210.1789 0003388 332.1578 27.9505 15.72342615426946
| Epoch (UTC): | 06 December 2023 19:31:34 |
| Eccentricity: | 0.0003388 |
| inclination: | 96.9651° |
| perigee height: | 350 km |
| apogee height: | 354 km |
| right ascension of ascending node: | 210.1789° |
| argument of perigee: | 332.1578° |
| revolutions per day: | 15.72342615 |
| mean anomaly at epoch: | 27.9505° |
| orbit number at epoch: | 42694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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