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 59302U 26145.38425718 +.00000000 +00000-0 +64505-5 0 00003
2 59302 43.0009 157.5882 0001269 273.0851 86.9856 15.27575945 09
| Epoch (UTC): | 25 May 2026 09:13:19 |
| Eccentricity: | 0.0001269 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.5882° |
| argument of perigee: | 273.0851° |
| revolutions per day: | 15.27575945 |
| mean anomaly at epoch: | 86.9856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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