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 22182.81066444 .00000017 00000-0 32900-4 0 9995
2 44909 82.5203 220.7374 0216204 286.2668 71.4749 12.79713754117340
| Epoch (UTC): | 01 July 2022 19:27:21 |
| Eccentricity: | 0.0216204 |
| inclination: | 82.5203° |
| perigee height: | 1175 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 220.7374° |
| argument of perigee: | 286.2668° |
| revolutions per day: | 12.79713754 |
| mean anomaly at epoch: | 71.4749° |
| orbit number at epoch: | 11734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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