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 61059U 26145.39896383 +.00000000 +00000-0 +12087-4 0 00003
2 61059 53.1591 293.3581 0000721 110.9817 249.1278 15.69707868 05
| Epoch (UTC): | 25 May 2026 09:34:30 |
| Eccentricity: | 0.0000721 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 293.3581° |
| argument of perigee: | 110.9817° |
| revolutions per day: | 15.69707868 |
| mean anomaly at epoch: | 249.1278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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