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 59369U 26145.47814174 +.00000000 +00000-0 +36186-4 0 00007
2 59369 43.0027 175.2081 0001297 261.9986 98.0719 15.27576871 07
| Epoch (UTC): | 25 May 2026 11:28:31 |
| Eccentricity: | 0.0001297 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.2081° |
| argument of perigee: | 261.9986° |
| revolutions per day: | 15.27576871 |
| mean anomaly at epoch: | 98.0719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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