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 26021.85808521 +.00000000 +00000-0 +22499-3 0 00008
2 11574 74.0680 177.7260 0015796 357.7637 2.3446 14.42315692 07
| Epoch (UTC): | 21 January 2026 20:35:38 |
| Eccentricity: | 0.0015796 |
| inclination: | 74.0680° |
| perigee height: | 740 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 177.7260° |
| argument of perigee: | 357.7637° |
| revolutions per day: | 14.42315692 |
| mean anomaly at epoch: | 2.3446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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