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 62775U 26145.52369758 +.00000000 +00000-0 +82911-3 0 00007
2 62775 53.1598 324.9428 0001632 72.0654 288.0526 15.34400045 05
| Epoch (UTC): | 25 May 2026 12:34:07 |
| Eccentricity: | 0.0001632 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 324.9428° |
| argument of perigee: | 72.0654° |
| revolutions per day: | 15.34400045 |
| mean anomaly at epoch: | 288.0526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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