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 59046U 26145.49860696 +.00000000 +00000-0 -18729-4 0 00005
2 59046 43.0004 309.9206 0001021 273.2351 86.8384 15.27574566 08
| Epoch (UTC): | 25 May 2026 11:57:59 |
| Eccentricity: | 0.0001021 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.9206° |
| argument of perigee: | 273.2351° |
| revolutions per day: | 15.27574566 |
| mean anomaly at epoch: | 86.8384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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