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 59761U 26145.40258998 +.00000000 +00000-0 +28907-6 0 00006
2 59761 53.1572 187.9719 0000979 52.9171 307.1936 15.69704487 05
| Epoch (UTC): | 25 May 2026 09:39:43 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1572° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 187.9719° |
| argument of perigee: | 52.9171° |
| revolutions per day: | 15.69704487 |
| mean anomaly at epoch: | 307.1936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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