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 59163U 26145.09834581 +.00000000 +00000-0 +31541-3 0 00000
2 59163 43.0043 35.3088 0001245 234.7447 125.3288 15.27553425 08
| Epoch (UTC): | 25 May 2026 02:21:37 |
| Eccentricity: | 0.0001245 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 35.3088° |
| argument of perigee: | 234.7447° |
| revolutions per day: | 15.27553425 |
| mean anomaly at epoch: | 125.3288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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