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 63324U 26145.46042188 +.00000000 +00000-0 +10624-2 0 00007
2 63324 43.0003 316.8446 0001260 271.9992 88.0716 15.27590596 09
| Epoch (UTC): | 25 May 2026 11:03:00 |
| Eccentricity: | 0.0001260 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.8446° |
| argument of perigee: | 271.9992° |
| revolutions per day: | 15.27590596 |
| mean anomaly at epoch: | 88.0716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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