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 19826U 26103.92156097 +.00000000 +00000-0 +53530-4 0 00000
2 19826 82.9531 330.6847 0031392 69.5716 301.3904 13.72547619 04
| Epoch (UTC): | 13 April 2026 22:07:02 |
| Eccentricity: | 0.0031392 |
| inclination: | 82.9531° |
| perigee height: | 967 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 330.6847° |
| argument of perigee: | 69.5716° |
| revolutions per day: | 13.72547619 |
| mean anomaly at epoch: | 301.3904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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