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 19419U 26106.52285799 +.00000000 +00000-0 +97762-4 0 00004
2 19419 90.0454 20.7048 0094117 250.1245 284.3396 13.42649003 07
| Epoch (UTC): | 16 April 2026 12:32:54 |
| Eccentricity: | 0.0094117 |
| inclination: | 90.0454° |
| perigee height: | 1029 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 20.7048° |
| argument of perigee: | 250.1245° |
| revolutions per day: | 13.42649003 |
| mean anomaly at epoch: | 284.3396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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