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 59112U 26145.39937572 +.00000000 +00000-0 +50717-3 0 00007
2 59112 97.5510 294.4330 0005867 278.7110 81.3480 15.56867388 05
| Epoch (UTC): | 25 May 2026 09:35:06 |
| Eccentricity: | 0.0005867 |
| inclination: | 97.5510° |
| perigee height: | 393 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 294.4330° |
| argument of perigee: | 278.7110° |
| revolutions per day: | 15.56867388 |
| mean anomaly at epoch: | 81.3480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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