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 19460U 26071.75591355 +.00000000 +00000-0 +69121-4 0 00002
2 19460 84.9918 169.1237 0004734 71.6130 288.5578 14.34416115 09
| Epoch (UTC): | 12 March 2026 18:08:30 |
| Eccentricity: | 0.0004734 |
| inclination: | 84.9918° |
| perigee height: | 774 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 169.1237° |
| argument of perigee: | 71.6130° |
| revolutions per day: | 14.34416115 |
| mean anomaly at epoch: | 288.5578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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