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 63075U 26145.60563279 +.00000000 +00000-0 +00000-0 0 00000
2 63075 0.0177 255.0415 0002932 234.6434 82.0383 1.00269699 08
| Epoch (UTC): | 25 May 2026 14:32:06 |
| Eccentricity: | 0.0002932 |
| inclination: | 0.0177° |
| perigee height: | 35775 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 255.0415° |
| argument of perigee: | 234.6434° |
| revolutions per day: | 1.00269699 |
| mean anomaly at epoch: | 82.0383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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