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 19345.60743776 +.00000106 +00000-0 +49713-4 0 9992
2 26094 100.2008 215.9990 0034290 137.6404 222.7436 14.42562131041776
| Epoch (UTC): | 11 December 2019 14:34:42 |
| Eccentricity: | 0.0034290 |
| inclination: | 100.2008° |
| perigee height: | 725 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 215.9990° |
| argument of perigee: | 137.6404° |
| revolutions per day: | 14.42562131 |
| mean anomaly at epoch: | 222.7436° |
| orbit number at epoch: | 4177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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