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 55346U 26145.56103410 +.00000000 +00000-0 +18284-4 0 00001
2 55346 43.0029 228.9539 0001908 273.2264 86.8370 15.27576350 08
| Epoch (UTC): | 25 May 2026 13:27:53 |
| Eccentricity: | 0.0001908 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 228.9539° |
| argument of perigee: | 273.2264° |
| revolutions per day: | 15.27576350 |
| mean anomaly at epoch: | 86.8370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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