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 55635U 26145.54716120 +.00000000 +00000-0 +59511-4 0 00006
2 55635 69.9991 350.6859 0002895 267.8622 92.2205 14.98339511 06
| Epoch (UTC): | 25 May 2026 13:07:54 |
| Eccentricity: | 0.0002895 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 350.6859° |
| argument of perigee: | 267.8622° |
| revolutions per day: | 14.98339511 |
| mean anomaly at epoch: | 92.2205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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