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 59168U 26145.39971443 +.00000000 +00000-0 -91583-5 0 00002
2 59168 43.0033 34.1269 0001186 272.9706 87.1010 15.27574630 05
| Epoch (UTC): | 25 May 2026 09:35:35 |
| Eccentricity: | 0.0001186 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 34.1269° |
| argument of perigee: | 272.9706° |
| revolutions per day: | 15.27574630 |
| mean anomaly at epoch: | 87.1010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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