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 54809U 26145.04987127 +.00000000 +00000-0 +35117-4 0 00006
2 54809 53.2127 45.8804 0001213 86.9555 273.1576 15.08842029 02
| Epoch (UTC): | 25 May 2026 01:11:48 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 45.8804° |
| argument of perigee: | 86.9555° |
| revolutions per day: | 15.08842029 |
| mean anomaly at epoch: | 273.1576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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