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 55357U 26145.51235411 +.00000000 +00000-0 +15775-4 0 00007
2 55357 43.0031 229.4411 0001541 269.6155 90.4520 15.27577645 05
| Epoch (UTC): | 25 May 2026 12:17:47 |
| Eccentricity: | 0.0001541 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.4411° |
| argument of perigee: | 269.6155° |
| revolutions per day: | 15.27577645 |
| mean anomaly at epoch: | 90.4520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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