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 11573U 26099.95936676 +.00000000 +00000-0 +53667-4 0 00008
2 11573 74.0679 191.8267 0016586 309.6022 50.3667 14.37603915 00
| Epoch (UTC): | 09 April 2026 23:01:29 |
| Eccentricity: | 0.0016586 |
| inclination: | 74.0679° |
| perigee height: | 755 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 191.8267° |
| argument of perigee: | 309.6022° |
| revolutions per day: | 14.37603915 |
| mean anomaly at epoch: | 50.3667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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