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 47158U 26145.27431127 +.00000000 +00000-0 +76824-3 0 00003
2 47158 53.0426 252.7294 0006557 2.7790 357.3263 15.73358041 02
| Epoch (UTC): | 25 May 2026 06:35:00 |
| Eccentricity: | 0.0006557 |
| inclination: | 53.0426° |
| perigee height: | 345 km |
| apogee height: | 354 km |
| right ascension of ascending node: | 252.7294° |
| argument of perigee: | 2.7790° |
| revolutions per day: | 15.73358041 |
| mean anomaly at epoch: | 357.3263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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