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 65597U 26145.46546715 +.00000000 +00000-0 +39360-3 0 00005
2 65597 97.4475 213.9630 0001831 163.9539 196.1746 15.05659188 05
| Epoch (UTC): | 25 May 2026 11:10:16 |
| Eccentricity: | 0.0001831 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9630° |
| argument of perigee: | 163.9539° |
| revolutions per day: | 15.05659188 |
| mean anomaly at epoch: | 196.1746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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