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 59505U 26145.34765126 +.00000000 +00000-0 +12163-3 0 00005
2 59505 43.0038 267.3191 0002089 242.1431 117.9210 15.27578574 01
| Epoch (UTC): | 25 May 2026 08:20:37 |
| Eccentricity: | 0.0002089 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 267.3191° |
| argument of perigee: | 242.1431° |
| revolutions per day: | 15.27578574 |
| mean anomaly at epoch: | 117.9210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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