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 59075U 26145.56653204 +.00000000 +00000-0 +89488-4 0 00009
2 59075 43.0008 236.1377 0000629 278.6188 81.4593 15.27583053 08
| Epoch (UTC): | 25 May 2026 13:35:48 |
| Eccentricity: | 0.0000629 |
| inclination: | 43.0008° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 236.1377° |
| argument of perigee: | 278.6188° |
| revolutions per day: | 15.27583053 |
| mean anomaly at epoch: | 81.4593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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