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 65751U 26145.54481709 +.00000000 +00000-0 +79771-3 0 00007
2 65751 53.1585 335.6757 0001020 68.8880 291.2229 15.30215129 06
| Epoch (UTC): | 25 May 2026 13:04:32 |
| Eccentricity: | 0.0001020 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.6757° |
| argument of perigee: | 68.8880° |
| revolutions per day: | 15.30215129 |
| mean anomaly at epoch: | 291.2229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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