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 63832U 26145.36968803 +.00000000 +00000-0 +74155-3 0 00001
2 63832 43.0003 99.3426 0001170 267.8506 92.2212 15.27601305 08
| Epoch (UTC): | 25 May 2026 08:52:21 |
| Eccentricity: | 0.0001170 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.3426° |
| argument of perigee: | 267.8506° |
| revolutions per day: | 15.27601305 |
| mean anomaly at epoch: | 92.2212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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