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 19071U 26103.70504301 +.00000000 +00000-0 +85067-4 0 00003
2 19071 90.3329 20.3660 0187244 187.4298 188.1190 13.27972292 00
| Epoch (UTC): | 13 April 2026 16:55:15 |
| Eccentricity: | 0.0187244 |
| inclination: | 90.3329° |
| perigee height: | 1013 km |
| apogee height: | 1295 km |
| right ascension of ascending node: | 20.3660° |
| argument of perigee: | 187.4298° |
| revolutions per day: | 13.27972292 |
| mean anomaly at epoch: | 188.1190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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