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 19257U 26064.63418508 +.00000000 +00000-0 +12839-3 0 00006
2 19257 74.0466 119.9422 0021348 299.8199 173.7495 14.38913126 00
| Epoch (UTC): | 05 March 2026 15:13:13 |
| Eccentricity: | 0.0021348 |
| inclination: | 74.0466° |
| perigee height: | 747 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 119.9422° |
| argument of perigee: | 299.8199° |
| revolutions per day: | 14.38913126 |
| mean anomaly at epoch: | 173.7495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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