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 26073.46194066 +.00000000 +00000-0 +10698-3 0 00002
2 11574 74.0667 82.2084 0017110 254.4139 105.5129 14.42354150 04
| Epoch (UTC): | 14 March 2026 11:05:11 |
| Eccentricity: | 0.0017110 |
| inclination: | 74.0667° |
| perigee height: | 739 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 82.2084° |
| argument of perigee: | 254.4139° |
| revolutions per day: | 14.42354150 |
| mean anomaly at epoch: | 105.5129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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