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 39430U 13066Q 22147.07447044 .00001997 00000-0 36228-3 0 9991
2 39430 97.8106 55.4937 0150663 112.0490 249.6780 14.60132996453170
| Epoch (UTC): | 27 May 2022 01:47:14 |
| Eccentricity: | 0.0150663 |
| inclination: | 97.8106° |
| perigee height: | 586 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 55.4937° |
| argument of perigee: | 112.0490° |
| revolutions per day: | 14.60132996 |
| mean anomaly at epoch: | 249.6780° |
| orbit number at epoch: | 45317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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