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 54206U 26145.54578575 +.00000000 +00000-0 +39723-4 0 00002
2 54206 53.2118 333.9358 0001193 89.7894 270.3235 15.08838143 05
| Epoch (UTC): | 25 May 2026 13:05:55 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 333.9358° |
| argument of perigee: | 89.7894° |
| revolutions per day: | 15.08838143 |
| mean anomaly at epoch: | 270.3235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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