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 54175U 26145.03934707 +.00000000 +00000-0 -25857-4 0 00008
2 54175 53.2138 21.3839 0001221 98.9019 261.2112 15.08846089 08
| Epoch (UTC): | 25 May 2026 00:56:39 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 21.3839° |
| argument of perigee: | 98.9019° |
| revolutions per day: | 15.08846089 |
| mean anomaly at epoch: | 261.2112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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