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 59835U 26145.15442723 +.00000000 +00000-0 +11740-4 0 00006
2 59835 43.0040 202.3164 0001856 273.3244 86.7396 15.27574929 06
| Epoch (UTC): | 25 May 2026 03:42:22 |
| Eccentricity: | 0.0001856 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 202.3164° |
| argument of perigee: | 273.3244° |
| revolutions per day: | 15.27574929 |
| mean anomaly at epoch: | 86.7396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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