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 59395U 26145.61126271 +.00000000 +00000-0 +39560-3 0 00004
2 59395 34.9983 267.8219 0003107 123.3238 236.7775 15.23064386 02
| Epoch (UTC): | 25 May 2026 14:40:13 |
| Eccentricity: | 0.0003107 |
| inclination: | 34.9983° |
| perigee height: | 494 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 267.8219° |
| argument of perigee: | 123.3238° |
| revolutions per day: | 15.23064386 |
| mean anomaly at epoch: | 236.7775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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