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 26065U 00004E 24279.43643341 .00001516 00000-0 51962-3 0 9994
2 26065 100.2298 93.4521 0036133 345.6328 14.3822 14.37734437294484
| Epoch (UTC): | 05 October 2024 10:28:27 |
| Eccentricity: | 0.0036133 |
| inclination: | 100.2298° |
| perigee height: | 740 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 93.4521° |
| argument of perigee: | 345.6328° |
| revolutions per day: | 14.37734437 |
| mean anomaly at epoch: | 14.3822° |
| orbit number at epoch: | 29448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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