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 54759U 26145.04903779 +.00000000 +00000-0 +18988-5 0 00009
2 54759 53.2136 56.5580 0001613 89.5163 270.6014 15.08837208 06
| Epoch (UTC): | 25 May 2026 01:10:36 |
| Eccentricity: | 0.0001613 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 56.5580° |
| argument of perigee: | 89.5163° |
| revolutions per day: | 15.08837208 |
| mean anomaly at epoch: | 270.6014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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