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 59694U 26145.61332193 +.00000000 +00000-0 +30563-4 0 00003
2 59694 43.0034 345.7287 0000904 267.9401 92.1347 15.27575476 02
| Epoch (UTC): | 25 May 2026 14:43:11 |
| Eccentricity: | 0.0000904 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.7287° |
| argument of perigee: | 267.9401° |
| revolutions per day: | 15.27575476 |
| mean anomaly at epoch: | 92.1347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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