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 59422U 26145.22079170 +.00000000 +00000-0 +59274-4 0 00002
2 59422 53.1591 76.5767 0000750 82.1167 277.9936 15.69709116 01
| Epoch (UTC): | 25 May 2026 05:17:56 |
| Eccentricity: | 0.0000750 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 76.5767° |
| argument of perigee: | 82.1167° |
| revolutions per day: | 15.69709116 |
| mean anomaly at epoch: | 277.9936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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