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 60359U 26145.17773877 +.00000000 +00000-0 +59214-4 0 00006
2 60359 53.1604 314.6568 0001016 86.0594 274.0523 15.30200966 02
| Epoch (UTC): | 25 May 2026 04:15:56 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.6568° |
| argument of perigee: | 86.0594° |
| revolutions per day: | 15.30200966 |
| mean anomaly at epoch: | 274.0523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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