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 31825U 99025CHP 22175.29429080 .00000656 00000-0 29998-3 0 9992
2 31825 98.6156 196.9102 0177504 37.1717 324.1595 14.16622381776490
| Epoch (UTC): | 24 June 2022 07:03:46 |
| Eccentricity: | 0.0177504 |
| inclination: | 98.6156° |
| perigee height: | 709 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 196.9102° |
| argument of perigee: | 37.1717° |
| revolutions per day: | 14.16622381 |
| mean anomaly at epoch: | 324.1595° |
| orbit number at epoch: | 77649 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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