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 30417U 99025AEG 22228.49033358 .00000250 00000-0 15558-3 0 9995
2 30417 98.6597 240.0748 0065582 347.0131 168.7098 14.12464834802355
| Epoch (UTC): | 16 August 2022 11:46:04 |
| Eccentricity: | 0.0065582 |
| inclination: | 98.6597° |
| perigee height: | 803 km |
| apogee height: | 898 km |
| right ascension of ascending node: | 240.0748° |
| argument of perigee: | 347.0131° |
| revolutions per day: | 14.12464834 |
| mean anomaly at epoch: | 168.7098° |
| orbit number at epoch: | 80235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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