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 63557U 26145.10736170 +.00000000 +00000-0 +12455-2 0 00001
2 63557 43.0019 53.4936 0002670 259.9327 100.1240 15.70925430 01
| Epoch (UTC): | 25 May 2026 02:34:36 |
| Eccentricity: | 0.0002670 |
| inclination: | 43.0019° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 53.4936° |
| argument of perigee: | 259.9327° |
| revolutions per day: | 15.70925430 |
| mean anomaly at epoch: | 100.1240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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