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 24339.91691451 .00000455 00000-0 18998-3 0 9998
2 22826 98.7609 34.1590 0007886 286.0592 73.9722 14.31073275627316
| Epoch (UTC): | 04 December 2024 22:00:21 |
| Eccentricity: | 0.0007886 |
| inclination: | 98.7609° |
| perigee height: | 782 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 34.1590° |
| argument of perigee: | 286.0592° |
| revolutions per day: | 14.31073275 |
| mean anomaly at epoch: | 73.9722° |
| orbit number at epoch: | 62731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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