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 19656U 26088.10846684 +.00000000 +00000-0 +12646-3 0 00003
2 19656 70.9824 347.0256 0212433 317.4633 41.0174 13.71924229 05
| Epoch (UTC): | 29 March 2026 02:36:11 |
| Eccentricity: | 0.0212433 |
| inclination: | 70.9824° |
| perigee height: | 836 km |
| apogee height: | 1149 km |
| right ascension of ascending node: | 347.0256° |
| argument of perigee: | 317.4633° |
| revolutions per day: | 13.71924229 |
| mean anomaly at epoch: | 41.0174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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