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 59399U 26145.59325507 +.00000000 +00000-0 +59907-4 0 00006
2 59399 43.0037 342.1699 0001107 274.3311 85.7414 15.27578584 09
| Epoch (UTC): | 25 May 2026 14:14:17 |
| Eccentricity: | 0.0001107 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1699° |
| argument of perigee: | 274.3311° |
| revolutions per day: | 15.27578584 |
| mean anomaly at epoch: | 85.7414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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