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 13778U 26020.96825325 +.00000000 +00000-0 +12364-3 0 00008
2 13778 100.0844 56.1977 0020392 321.2544 38.7159 14.09679976 08
| Epoch (UTC): | 20 January 2026 23:14:17 |
| Eccentricity: | 0.0020392 |
| inclination: | 100.0844° |
| perigee height: | 846 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 56.1977° |
| argument of perigee: | 321.2544° |
| revolutions per day: | 14.09679976 |
| mean anomaly at epoch: | 38.7159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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