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 62291U 26145.58837227 +.00000000 +00000-0 +96037-4 0 00002
2 62291 59.9187 319.1690 0007350 92.2244 267.9605 13.75201788 05
| Epoch (UTC): | 25 May 2026 14:07:15 |
| Eccentricity: | 0.0007350 |
| inclination: | 59.9187° |
| perigee height: | 976 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 319.1690° |
| argument of perigee: | 92.2244° |
| revolutions per day: | 13.75201788 |
| mean anomaly at epoch: | 267.9605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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