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 26045.88008550 +.00000000 +00000-0 +10676-1 0 00000
2 59588 97.2190 352.1195 0046978 145.2118 215.2132 13.88621345 04
| Epoch (UTC): | 14 February 2026 21:07:19 |
| Eccentricity: | 0.0046978 |
| inclination: | 97.2190° |
| perigee height: | 899 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 352.1195° |
| argument of perigee: | 145.2118° |
| revolutions per day: | 13.88621345 |
| mean anomaly at epoch: | 215.2132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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