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 63636U 26145.46242106 +.00000000 +00000-0 +78175-3 0 00001
2 63636 43.0001 292.0366 0001218 242.6392 117.4336 15.27590867 07
| Epoch (UTC): | 25 May 2026 11:05:53 |
| Eccentricity: | 0.0001218 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 292.0366° |
| argument of perigee: | 242.6392° |
| revolutions per day: | 15.27590867 |
| mean anomaly at epoch: | 117.4336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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