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 25397U 98043D 22222.40077871 .00000007 00000-0 22859-4 0 9991
2 25397 98.8205 173.0206 0000941 10.5593 349.5605 14.23764886251320
| Epoch (UTC): | 10 August 2022 09:37:07 |
| Eccentricity: | 0.0000941 |
| inclination: | 98.8205° |
| perigee height: | 812 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 173.0206° |
| argument of perigee: | 10.5593° |
| revolutions per day: | 14.23764886 |
| mean anomaly at epoch: | 349.5605° |
| orbit number at epoch: | 25132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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