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 54808U 26145.09732860 +.00000000 +00000-0 +33549-4 0 00009
2 54808 53.2126 31.2823 0001520 81.5458 278.5707 15.08834267 04
| Epoch (UTC): | 25 May 2026 02:20:09 |
| Eccentricity: | 0.0001520 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 31.2823° |
| argument of perigee: | 81.5458° |
| revolutions per day: | 15.08834267 |
| mean anomaly at epoch: | 278.5707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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