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 59130U 26145.66440808 +.00000000 +00000-0 +29105-3 0 00005
2 59130 97.5561 289.3217 0006465 299.7014 60.3589 15.42258326 07
| Epoch (UTC): | 25 May 2026 15:56:44 |
| Eccentricity: | 0.0006465 |
| inclination: | 97.5561° |
| perigee height: | 435 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 289.3217° |
| argument of perigee: | 299.7014° |
| revolutions per day: | 15.42258326 |
| mean anomaly at epoch: | 60.3589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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