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 62563U 26144.98766610 +.00000000 +00000-0 +13452-2 0 00002
2 62563 43.0049 39.8530 0002962 259.7538 100.2996 15.70860927 02
| Epoch (UTC): | 24 May 2026 23:42:14 |
| Eccentricity: | 0.0002962 |
| inclination: | 43.0049° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 39.8530° |
| argument of perigee: | 259.7538° |
| revolutions per day: | 15.70860927 |
| mean anomaly at epoch: | 100.2996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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