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 59554U 26145.57994174 +.00000000 +00000-0 +60767-4 0 00005
2 59554 42.9998 233.2547 0001417 265.6865 94.3824 15.27578325 03
| Epoch (UTC): | 25 May 2026 13:55:06 |
| Eccentricity: | 0.0001417 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 233.2547° |
| argument of perigee: | 265.6865° |
| revolutions per day: | 15.27578325 |
| mean anomaly at epoch: | 94.3824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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