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 data is extracted from the following two-line orbital elements,
1 26094U 00004M 18343.89291435 .00000058 00000-0 35263-4 0 9991
2 26094 100.2114 137.4052 0034593 101.9770 258.5295 14.42465955988931
| Epoch (UTC): | 09 December 2018 21:25:47 |
| Eccentricity: | 0.0034593 |
| inclination: | 100.2114° |
| perigee height: | 726 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 137.4052° |
| argument of perigee: | 101.9770° |
| revolutions per day: | 14.42465955 |
| mean anomaly at epoch: | 258.5295° |
| orbit number at epoch: | 98893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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