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 31698U 07026A 22175.63580503 -.00000748 00000-0 -32457-4 0 9995
2 31698 97.4451 183.1313 0001901 68.0157 69.3725 15.19144666833208
| Epoch (UTC): | 24 June 2022 15:15:33 |
| Eccentricity: | 0.0001901 |
| inclination: | 97.4451° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 183.1313° |
| argument of perigee: | 68.0157° |
| revolutions per day: | 15.19144666 |
| mean anomaly at epoch: | 69.3725° |
| orbit number at epoch: | 83320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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