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 59459U 26145.50279507 +.00000000 +00000-0 -26135-5 0 00001
2 59459 43.0006 316.9726 0001070 275.7432 84.3298 15.27571520 08
| Epoch (UTC): | 25 May 2026 12:04:01 |
| Eccentricity: | 0.0001070 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9726° |
| argument of perigee: | 275.7432° |
| revolutions per day: | 15.27571520 |
| mean anomaly at epoch: | 84.3298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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