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 63366U 26145.18745485 +.00000000 +00000-0 +46291-3 0 00002
2 63366 53.1583 56.9940 0001078 88.3475 271.7649 15.30208221 05
| Epoch (UTC): | 25 May 2026 04:29:56 |
| Eccentricity: | 0.0001078 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 56.9940° |
| argument of perigee: | 88.3475° |
| revolutions per day: | 15.30208221 |
| mean anomaly at epoch: | 271.7649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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