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 54090U 26145.58307559 +.00000000 +00000-0 -14457-3 0 00006
2 54090 53.2139 348.8395 0001231 112.3213 247.7909 15.08834696 01
| Epoch (UTC): | 25 May 2026 13:59:37 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.8395° |
| argument of perigee: | 112.3213° |
| revolutions per day: | 15.08834696 |
| mean anomaly at epoch: | 247.7909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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