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 26017.19011230 +.00000000 +00000-0 +14087-3 0 00002
2 19120 71.0137 177.4420 0019882 55.5101 304.7898 14.19606476 07
| Epoch (UTC): | 17 January 2026 04:33:45 |
| Eccentricity: | 0.0019882 |
| inclination: | 71.0137° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 177.4420° |
| argument of perigee: | 55.5101° |
| revolutions per day: | 14.19606476 |
| mean anomaly at epoch: | 304.7898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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