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 65762U 26145.52143914 +.00000000 +00000-0 +58491-4 0 00007
2 65762 51.8975 73.3089 0000846 99.2883 260.8175 14.79933816 00
| Epoch (UTC): | 25 May 2026 12:30:52 |
| Eccentricity: | 0.0000846 |
| inclination: | 51.8975° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 73.3089° |
| argument of perigee: | 99.2883° |
| revolutions per day: | 14.79933816 |
| mean anomaly at epoch: | 260.8175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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