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 59660U 26145.19809183 +.00000000 +00000-0 +43211-3 0 00000
2 59660 43.0006 326.3013 0001369 274.8633 85.2063 15.27600073 06
| Epoch (UTC): | 25 May 2026 04:45:15 |
| Eccentricity: | 0.0001369 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 326.3013° |
| argument of perigee: | 274.8633° |
| revolutions per day: | 15.27600073 |
| mean anomaly at epoch: | 85.2063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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