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 59766U 26145.09406147 +.00000000 +00000-0 -30337-4 0 00006
2 59766 53.1613 29.0635 0001069 93.7034 266.4089 15.30205533 03
| Epoch (UTC): | 25 May 2026 02:15:26 |
| Eccentricity: | 0.0001069 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.0635° |
| argument of perigee: | 93.7034° |
| revolutions per day: | 15.30205533 |
| mean anomaly at epoch: | 266.4089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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