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 63492U 26107.15322792 +.00000000 +00000-0 +13735-2 0 00005
2 63492 97.3903 9.3935 0003547 91.0317 269.1353 15.71953326 07
| Epoch (UTC): | 17 April 2026 03:40:38 |
| Eccentricity: | 0.0003547 |
| inclination: | 97.3903° |
| perigee height: | 351 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 9.3935° |
| argument of perigee: | 91.0317° |
| revolutions per day: | 15.71953326 |
| mean anomaly at epoch: | 269.1353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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