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 19120U 26022.47484329 +.00000000 +00000-0 +33563-4 0 00003
2 19120 71.0142 166.2680 0020096 46.7641 313.5158 14.19608473 03
| Epoch (UTC): | 22 January 2026 11:23:46 |
| Eccentricity: | 0.0020096 |
| inclination: | 71.0142° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 166.2680° |
| argument of perigee: | 46.7641° |
| revolutions per day: | 14.19608473 |
| mean anomaly at epoch: | 313.5158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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