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 19071U 26106.65422676 +.00000000 +00000-0 +97142-4 0 00001
2 19071 90.3330 20.4611 0187510 179.2121 247.2932 13.27972603 06
| Epoch (UTC): | 16 April 2026 15:42:05 |
| Eccentricity: | 0.0187510 |
| inclination: | 90.3330° |
| perigee height: | 1013 km |
| apogee height: | 1296 km |
| right ascension of ascending node: | 20.4611° |
| argument of perigee: | 179.2121° |
| revolutions per day: | 13.27972603 |
| mean anomaly at epoch: | 247.2932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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