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 26018.66983824 +.00000000 +00000-0 +12501-3 0 00001
2 19120 71.0139 174.3133 0019954 53.0773 307.2177 14.19607091 06
| Epoch (UTC): | 18 January 2026 16:04:34 |
| Eccentricity: | 0.0019954 |
| inclination: | 71.0139° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 174.3133° |
| argument of perigee: | 53.0773° |
| revolutions per day: | 14.19607091 |
| mean anomaly at epoch: | 307.2177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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