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 25940U 99057A 22222.43704547 .00000097 00000-0 49352-4 0 9997
2 25940 98.7087 181.0713 0004927 175.4149 184.7082 14.35649880195570
| Epoch (UTC): | 10 August 2022 10:29:20 |
| Eccentricity: | 0.0004927 |
| inclination: | 98.7087° |
| perigee height: | 769 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 181.0713° |
| argument of perigee: | 175.4149° |
| revolutions per day: | 14.35649880 |
| mean anomaly at epoch: | 184.7082° |
| orbit number at epoch: | 19557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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