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 41622U 16041A 23272.51773845 -.00000163 00000-0 00000-0 0 9994
2 41622 4.5079 297.8430 0200763 247.2751 264.3189 1.00271657 27147
| Epoch (UTC): | 29 September 2023 12:25:32 |
| Eccentricity: | 0.0200763 |
| inclination: | 4.5079° |
| perigee height: | 34940 km |
| apogee height: | 36633 km |
| right ascension of ascending node: | 297.8430° |
| argument of perigee: | 247.2751° |
| revolutions per day: | 1.00271657 |
| mean anomaly at epoch: | 264.3189° |
| orbit number at epoch: | 2714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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