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 55396U 26145.49568066 +.00000000 +00000-0 -19698-4 0 00001
2 55396 69.9992 230.6600 0003383 267.7835 92.2936 14.98328524 03
| Epoch (UTC): | 25 May 2026 11:53:46 |
| Eccentricity: | 0.0003383 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.6600° |
| argument of perigee: | 267.7835° |
| revolutions per day: | 14.98328524 |
| mean anomaly at epoch: | 92.2936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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