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 59474U 26145.51098326 +.00000000 +00000-0 +21737-5 0 00009
2 59474 43.0024 313.5574 0000927 281.5910 78.4838 15.27577697 00
| Epoch (UTC): | 25 May 2026 12:15:48 |
| Eccentricity: | 0.0000927 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.5574° |
| argument of perigee: | 281.5910° |
| revolutions per day: | 15.27577697 |
| mean anomaly at epoch: | 78.4838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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