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 59726U 26145.37418580 +.00000000 +00000-0 +54636-4 0 00004
2 59726 53.1601 143.6669 0001175 91.5415 268.5721 15.31692827 06
| Epoch (UTC): | 25 May 2026 08:58:49 |
| Eccentricity: | 0.0001175 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 143.6669° |
| argument of perigee: | 91.5415° |
| revolutions per day: | 15.31692827 |
| mean anomaly at epoch: | 268.5721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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