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 is defined by the following mean orbital elements,
1 22565U 26160.20283027 +.00000000 +00000-0 +28434-4 0 00007
2 22565 70.7612 329.7549 0009071 268.6811 91.3270 14.12366935 05
| Epoch (UTC): | 09 June 2026 04:52:04 |
| Eccentricity: | 0.0009071 |
| inclination: | 70.7612° |
| perigee height: | 845 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 329.7549° |
| argument of perigee: | 268.6811° |
| revolutions per day: | 14.12366935 |
| mean anomaly at epoch: | 91.3270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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