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 55305U 26145.52443522 +.00000000 +00000-0 -53243-3 0 00007
2 55305 69.9991 190.9146 0003910 265.2106 94.8606 14.98347646 03
| Epoch (UTC): | 25 May 2026 12:35:11 |
| Eccentricity: | 0.0003910 |
| inclination: | 69.9991° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.9146° |
| argument of perigee: | 265.2106° |
| revolutions per day: | 14.98347646 |
| mean anomaly at epoch: | 94.8606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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