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 55292U 26145.42011405 +.00000000 +00000-0 -12067-5 0 00003
2 55292 69.9965 190.9429 0004165 280.5060 79.5630 14.98325972 00
| Epoch (UTC): | 25 May 2026 10:04:57 |
| Eccentricity: | 0.0004165 |
| inclination: | 69.9965° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.9429° |
| argument of perigee: | 280.5060° |
| revolutions per day: | 14.98325972 |
| mean anomaly at epoch: | 79.5630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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