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 26609U 00072B 24279.43993662 -.00000111 00000-0 00000+0 0 9991
2 26609 7.3570 79.5598 7988051 348.4322 0.5051 1.25588931109861
| Epoch (UTC): | 05 October 2024 10:33:30 |
| Eccentricity: | 0.7988051 |
| inclination: | 7.3570° |
| perigee height: | 923 km |
| apogee height: | 58897 km |
| right ascension of ascending node: | 79.5598° |
| argument of perigee: | 348.4322° |
| revolutions per day: | 1.25588931 |
| mean anomaly at epoch: | 0.5051° |
| orbit number at epoch: | 10986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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