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 63503U 26145.33819436 +.00000000 +00000-0 -82437-1 0 00001
2 63503 53.1574 143.9976 0016463 75.2481 285.0346 15.38416024 02
| Epoch (UTC): | 25 May 2026 08:06:59 |
| Eccentricity: | 0.0016463 |
| inclination: | 53.1574° |
| perigee height: | 440 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 143.9976° |
| argument of perigee: | 75.2481° |
| revolutions per day: | 15.38416024 |
| mean anomaly at epoch: | 285.0346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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