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 59907U 26145.31858894 +.00000000 +00000-0 +25167-2 0 00000
2 59907 42.9943 9.9168 0021720 255.0382 104.8073 15.49972008 01
| Epoch (UTC): | 25 May 2026 07:38:46 |
| Eccentricity: | 0.0021720 |
| inclination: | 42.9943° |
| perigee height: | 402 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 9.9168° |
| argument of perigee: | 255.0382° |
| revolutions per day: | 15.49972008 |
| mean anomaly at epoch: | 104.8073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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