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 26070.75692845 +.00000000 +00000-0 +10333-3 0 00005
2 11574 74.0667 87.2163 0017134 259.6606 100.2619 14.42352142 04
| Epoch (UTC): | 11 March 2026 18:09:58 |
| Eccentricity: | 0.0017134 |
| inclination: | 74.0667° |
| perigee height: | 739 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 87.2163° |
| argument of perigee: | 259.6606° |
| revolutions per day: | 14.42352142 |
| mean anomaly at epoch: | 100.2619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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