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 61058U 26144.83085278 +.00000000 +00000-0 +88043-5 0 00009
2 61058 53.1586 296.2131 0000760 100.8248 259.2856 15.69699730 02
| Epoch (UTC): | 24 May 2026 19:56:25 |
| Eccentricity: | 0.0000760 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 296.2131° |
| argument of perigee: | 100.8248° |
| revolutions per day: | 15.69699730 |
| mean anomaly at epoch: | 259.2856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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