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 59405U 26145.54572597 +.00000000 +00000-0 -19276-4 0 00008
2 59405 43.0012 341.8085 0001195 245.6037 114.4690 15.27565969 07
| Epoch (UTC): | 25 May 2026 13:05:50 |
| Eccentricity: | 0.0001195 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.8085° |
| argument of perigee: | 245.6037° |
| revolutions per day: | 15.27565969 |
| mean anomaly at epoch: | 114.4690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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