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 59892U 26145.40859725 +.00000000 +00000-0 -64408-5 0 00002
2 59892 43.0016 44.8962 0000834 279.8901 80.1857 15.27580202 04
| Epoch (UTC): | 25 May 2026 09:48:22 |
| Eccentricity: | 0.0000834 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.8962° |
| argument of perigee: | 279.8901° |
| revolutions per day: | 15.27580202 |
| mean anomaly at epoch: | 80.1857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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