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 59479U 26145.09906862 +.00000000 +00000-0 +00000-0 0 00005
2 59479 2.0677 81.6776 0051213 133.9295 226.1281 0.98609711 00
| Epoch (UTC): | 25 May 2026 02:22:39 |
| Eccentricity: | 0.0051213 |
| inclination: | 2.0677° |
| perigee height: | 36041 km |
| apogee height: | 36477 km |
| right ascension of ascending node: | 81.6776° |
| argument of perigee: | 133.9295° |
| revolutions per day: | 0.98609711 |
| mean anomaly at epoch: | 226.1281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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