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 59476U 26145.52286698 +.00000000 +00000-0 +30509-4 0 00009
2 59476 43.0019 320.5768 0001376 266.4620 93.6074 15.27575426 07
| Epoch (UTC): | 25 May 2026 12:32:55 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.5768° |
| argument of perigee: | 266.4620° |
| revolutions per day: | 15.27575426 |
| mean anomaly at epoch: | 93.6074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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