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 62556U 26145.40103117 +.00000000 +00000-0 +19018-2 0 00003
2 62556 43.0009 37.8147 0000931 19.6338 340.4565 15.70892733 07
| Epoch (UTC): | 25 May 2026 09:37:29 |
| Eccentricity: | 0.0000931 |
| inclination: | 43.0009° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 37.8147° |
| argument of perigee: | 19.6338° |
| revolutions per day: | 15.70892733 |
| mean anomaly at epoch: | 340.4565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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