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 11574U 26161.61606647 +.00000000 +00000-0 +65998-4 0 00004
2 11574 74.0695 279.0214 0014870 65.4469 294.8235 14.42401070 06
| Epoch (UTC): | 10 June 2026 14:47:08 |
| Eccentricity: | 0.0014870 |
| inclination: | 74.0695° |
| perigee height: | 740 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 279.0214° |
| argument of perigee: | 65.4469° |
| revolutions per day: | 14.42401070 |
| mean anomaly at epoch: | 294.8235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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