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 41590U 16038C 23222.63508522 -.00000706 78143-6 00000+0 0 9991
2 41590 20.6186 198.6455 8117029 255.9094 11.8908 1.34182029 30868
| Epoch (UTC): | 10 August 2023 15:14:31 |
| Eccentricity: | 0.8117029 |
| inclination: | 20.6186° |
| perigee height: | 160 km |
| apogee height: | 56527 km |
| right ascension of ascending node: | 198.6455° |
| argument of perigee: | 255.9094° |
| revolutions per day: | 1.34182029 |
| mean anomaly at epoch: | 11.8908° |
| orbit number at epoch: | 3086 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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