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 59588U 26065.40162319 +.00000000 +00000-0 +22568-1 0 00007
2 59588 97.2094 7.2527 0057270 85.3402 275.4299 13.89441729 00
| Epoch (UTC): | 06 March 2026 09:38:20 |
| Eccentricity: | 0.0057270 |
| inclination: | 97.2094° |
| perigee height: | 889 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 7.2527° |
| argument of perigee: | 85.3402° |
| revolutions per day: | 13.89441729 |
| mean anomaly at epoch: | 275.4299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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