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 19120U 26065.31624693 +.00000000 +00000-0 -35907-4 0 00008
2 19120 71.0131 75.6814 0022569 339.2734 20.7473 14.19615649 03
| Epoch (UTC): | 06 March 2026 07:35:23 |
| Eccentricity: | 0.0022569 |
| inclination: | 71.0131° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 75.6814° |
| argument of perigee: | 339.2734° |
| revolutions per day: | 14.19615649 |
| mean anomaly at epoch: | 20.7473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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