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 59667U 26145.50702845 +.00000000 +00000-0 +10281-3 0 00000
2 59667 42.9996 324.3174 0001585 272.6904 87.3767 15.27581139 07
| Epoch (UTC): | 25 May 2026 12:10:07 |
| Eccentricity: | 0.0001585 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.3174° |
| argument of perigee: | 272.6904° |
| revolutions per day: | 15.27581139 |
| mean anomaly at epoch: | 87.3767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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