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 55690U 26145.62375020 +.00000000 +00000-0 +23525-3 0 00001
2 55690 97.3467 220.6913 0001386 137.6459 222.4885 15.23319937 03
| Epoch (UTC): | 25 May 2026 14:58:12 |
| Eccentricity: | 0.0001386 |
| inclination: | 97.3467° |
| perigee height: | 495 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 220.6913° |
| argument of perigee: | 137.6459° |
| revolutions per day: | 15.23319937 |
| mean anomaly at epoch: | 222.4885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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