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 26019.16308001 +.00000000 +00000-0 +10728-3 0 00004
2 19120 71.0139 173.2704 0019975 52.2253 308.0678 14.19607195 05
| Epoch (UTC): | 19 January 2026 03:54:50 |
| Eccentricity: | 0.0019975 |
| inclination: | 71.0139° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 173.2704° |
| argument of perigee: | 52.2253° |
| revolutions per day: | 14.19607195 |
| mean anomaly at epoch: | 308.0678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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