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 25693U 99021A 22222.11091902 .00000122 00000-0 34336-4 0 9997
2 25693 64.5554 90.3325 0038697 235.2714 124.4745 14.81160113258542
| Epoch (UTC): | 10 August 2022 02:39:43 |
| Eccentricity: | 0.0038697 |
| inclination: | 64.5554° |
| perigee height: | 598 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 90.3325° |
| argument of perigee: | 235.2714° |
| revolutions per day: | 14.81160113 |
| mean anomaly at epoch: | 124.4745° |
| orbit number at epoch: | 25854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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