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 22565U 93016A 25342.33709034 -.00000170 00000-0 -65665-4 0 9996
2 22565 70.7706 356.6998 0006732 214.3518 145.7168 14.12390855686401
| Epoch (UTC): | 08 December 2025 08:05:24 |
| Eccentricity: | 0.0006732 |
| inclination: | 70.7706° |
| perigee height: | 846 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 356.6998° |
| argument of perigee: | 214.3518° |
| revolutions per day: | 14.12390855 |
| mean anomaly at epoch: | 145.7168° |
| orbit number at epoch: | 68640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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