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 24280.62558704 .00000839 00000-0 33602-3 0 9999
2 22826 98.7703 334.3677 0009954 97.6268 262.6046 14.30997492618834
| Epoch (UTC): | 06 October 2024 15:00:50 |
| Eccentricity: | 0.0009954 |
| inclination: | 98.7703° |
| perigee height: | 781 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 334.3677° |
| argument of perigee: | 97.6268° |
| revolutions per day: | 14.30997492 |
| mean anomaly at epoch: | 262.6046° |
| orbit number at epoch: | 61883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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