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 54091U 26145.55358438 +.00000000 +00000-0 +13906-3 0 00003
2 54091 53.2125 348.6608 0001349 94.1502 265.9644 15.08826574 04
| Epoch (UTC): | 25 May 2026 13:17:09 |
| Eccentricity: | 0.0001349 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.6608° |
| argument of perigee: | 94.1502° |
| revolutions per day: | 15.08826574 |
| mean anomaly at epoch: | 265.9644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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