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 59781U 26145.58226427 +.00000000 +00000-0 +68038-4 0 00006
2 59781 98.6672 264.6481 0010964 276.7208 83.2728 14.31837257 04
| Epoch (UTC): | 25 May 2026 13:58:27 |
| Eccentricity: | 0.0010964 |
| inclination: | 98.6672° |
| perigee height: | 778 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 264.6481° |
| argument of perigee: | 276.7208° |
| revolutions per day: | 14.31837257 |
| mean anomaly at epoch: | 83.2728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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