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 54064U 26145.47040493 +.00000000 +00000-0 +10887-3 0 00008
2 54064 53.2149 314.6185 0001159 90.4447 269.6678 15.08832722 09
| Epoch (UTC): | 25 May 2026 11:17:22 |
| Eccentricity: | 0.0001159 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.6185° |
| argument of perigee: | 90.4447° |
| revolutions per day: | 15.08832722 |
| mean anomaly at epoch: | 269.6678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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