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 63383U 26145.20225047 +.00000000 +00000-0 +11752-2 0 00004
2 63383 53.1574 67.7330 0001169 98.1353 261.9780 15.30210485 04
| Epoch (UTC): | 25 May 2026 04:51:14 |
| Eccentricity: | 0.0001169 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 67.7330° |
| argument of perigee: | 98.1353° |
| revolutions per day: | 15.30210485 |
| mean anomaly at epoch: | 261.9780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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