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 41789U 16059G 22175.79669457 .00000566 00000-0 11446-3 0 9996
2 41789 97.9155 221.6450 0029309 131.8786 228.4908 14.64697942306941
| Epoch (UTC): | 24 June 2022 19:07:14 |
| Eccentricity: | 0.0029309 |
| inclination: | 97.9155° |
| perigee height: | 657 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 221.6450° |
| argument of perigee: | 131.8786° |
| revolutions per day: | 14.64697942 |
| mean anomaly at epoch: | 228.4908° |
| orbit number at epoch: | 30694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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