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 59363U 26145.52776875 +.00000000 +00000-0 -23544-6 0 00009
2 59363 43.0032 179.0332 0001624 279.6537 80.4132 15.27576747 06
| Epoch (UTC): | 25 May 2026 12:39:59 |
| Eccentricity: | 0.0001624 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 179.0332° |
| argument of perigee: | 279.6537° |
| revolutions per day: | 15.27576747 |
| mean anomaly at epoch: | 80.4132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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