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 63577U 26145.56145385 +.00000000 +00000-0 +10047-2 0 00000
2 63577 43.0007 247.8517 0001841 273.4366 86.6275 15.27601164 00
| Epoch (UTC): | 25 May 2026 13:28:29 |
| Eccentricity: | 0.0001841 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.8517° |
| argument of perigee: | 273.4366° |
| revolutions per day: | 15.27601164 |
| mean anomaly at epoch: | 86.6275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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