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 65569U 26145.38055851 +.00000000 +00000-0 +73856-4 0 00000
2 65569 81.3072 32.0699 0004825 251.1106 108.9527 13.83404287 00
| Epoch (UTC): | 25 May 2026 09:08:00 |
| Eccentricity: | 0.0004825 |
| inclination: | 81.3072° |
| perigee height: | 948 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 32.0699° |
| argument of perigee: | 251.1106° |
| revolutions per day: | 13.83404287 |
| mean anomaly at epoch: | 108.9527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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