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 63175U 26145.55716325 +.00000000 +00000-0 +17517-4 0 00002
2 63175 88.9691 303.0575 0016917 19.1928 340.9857 13.51012730 01
| Epoch (UTC): | 25 May 2026 13:22:18 |
| Eccentricity: | 0.0016917 |
| inclination: | 88.9691° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 303.0575° |
| argument of perigee: | 19.1928° |
| revolutions per day: | 13.51012730 |
| mean anomaly at epoch: | 340.9857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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