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 26044.79924516 +.00000000 +00000-0 +16918-1 0 00003
2 59588 97.2195 351.2822 0046651 148.9595 211.4340 13.88605461 03
| Epoch (UTC): | 13 February 2026 19:10:54 |
| Eccentricity: | 0.0046651 |
| inclination: | 97.2195° |
| perigee height: | 899 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 351.2822° |
| argument of perigee: | 148.9595° |
| revolutions per day: | 13.88605461 |
| mean anomaly at epoch: | 211.4340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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