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 22826U 93061D 24285.38019109 .00003933 00000-0 15097-2 0 9993
2 22826 98.7695 339.1646 0010032 85.1378 275.0949 14.31026721619511
| Epoch (UTC): | 11 October 2024 09:07:28 |
| Eccentricity: | 0.0010032 |
| inclination: | 98.7695° |
| perigee height: | 781 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 339.1646° |
| argument of perigee: | 85.1378° |
| revolutions per day: | 14.31026721 |
| mean anomaly at epoch: | 275.0949° |
| orbit number at epoch: | 61951 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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