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 26017.90450028 +.00000000 +00000-0 +12197-3 0 00008
2 11574 74.0676 185.0435 0015613 6.1774 353.9572 14.42310003 09
| Epoch (UTC): | 17 January 2026 21:42:28 |
| Eccentricity: | 0.0015613 |
| inclination: | 74.0676° |
| perigee height: | 740 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 185.0435° |
| argument of perigee: | 6.1774° |
| revolutions per day: | 14.42310003 |
| mean anomaly at epoch: | 353.9572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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