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 44909U 19096E 22179.52703961 .00000028 00000-0 75692-4 0 9998
2 44909 82.5206 222.9188 0216253 293.9847 63.8748 12.79713638116926
| Epoch (UTC): | 28 June 2022 12:38:56 |
| Eccentricity: | 0.0216253 |
| inclination: | 82.5206° |
| perigee height: | 1175 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 222.9188° |
| argument of perigee: | 293.9847° |
| revolutions per day: | 12.79713638 |
| mean anomaly at epoch: | 63.8748° |
| orbit number at epoch: | 11692 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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