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 59401U 26144.64443559 +.00000000 +00000-0 -48201-4 0 00009
2 59401 43.0009 347.0833 0001240 265.0040 95.0670 15.27574138 09
| Epoch (UTC): | 24 May 2026 15:27:59 |
| Eccentricity: | 0.0001240 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 347.0833° |
| argument of perigee: | 265.0040° |
| revolutions per day: | 15.27574138 |
| mean anomaly at epoch: | 95.0670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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