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 61551U 26145.34914740 +.00000000 +00000-0 +53736-4 0 00009
2 61551 53.1614 17.8841 0000865 92.4746 267.6356 15.34391766 00
| Epoch (UTC): | 25 May 2026 08:22:46 |
| Eccentricity: | 0.0000865 |
| inclination: | 53.1614° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 17.8841° |
| argument of perigee: | 92.4746° |
| revolutions per day: | 15.34391766 |
| mean anomaly at epoch: | 267.6356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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