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 58708U 26145.57344125 +.00000000 +00000-0 +28048-4 0 00006
2 58708 53.1593 254.9440 0001093 91.9547 268.1597 15.69693137 00
| Epoch (UTC): | 25 May 2026 13:45:45 |
| Eccentricity: | 0.0001093 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 254.9440° |
| argument of perigee: | 91.9547° |
| revolutions per day: | 15.69693137 |
| mean anomaly at epoch: | 268.1597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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