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 58706U 26145.35298976 +.00000000 +00000-0 +37599-4 0 00003
2 58706 53.1601 255.7028 0001013 60.8527 299.2592 15.69725916 05
| Epoch (UTC): | 25 May 2026 08:28:18 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.1601° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 255.7028° |
| argument of perigee: | 60.8527° |
| revolutions per day: | 15.69725916 |
| mean anomaly at epoch: | 299.2592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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