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 63036U 26145.35452560 +.00000000 +00000-0 +38256-3 0 00006
2 63036 53.1574 262.0912 0001153 94.0891 266.0241 15.30211617 06
| Epoch (UTC): | 25 May 2026 08:30:31 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 262.0912° |
| argument of perigee: | 94.0891° |
| revolutions per day: | 15.30211617 |
| mean anomaly at epoch: | 266.0241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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