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 19070U 26053.85773234 +.00000000 +00000-0 +20098-3 0 00007
2 19070 90.3266 18.6333 0188951 340.4590 35.9122 13.27800934 05
| Epoch (UTC): | 22 February 2026 20:35:08 |
| Eccentricity: | 0.0188951 |
| inclination: | 90.3266° |
| perigee height: | 1013 km |
| apogee height: | 1297 km |
| right ascension of ascending node: | 18.6333° |
| argument of perigee: | 340.4590° |
| revolutions per day: | 13.27800934 |
| mean anomaly at epoch: | 35.9122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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