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 59473U 26145.51130220 +.00000000 +00000-0 +59809-4 0 00008
2 59473 43.0011 320.4919 0001147 265.6396 94.4325 15.27575903 08
| Epoch (UTC): | 25 May 2026 12:16:16 |
| Eccentricity: | 0.0001147 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.4919° |
| argument of perigee: | 265.6396° |
| revolutions per day: | 15.27575903 |
| mean anomaly at epoch: | 94.4325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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