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 26093U 00004L 19340.76906425 +.00000280 +00000-0 +85329-4 0 9991
2 26093 100.1902 287.7514 0030338 319.5649 040.3285 14.51705286045733
| Epoch (UTC): | 06 December 2019 18:27:27 |
| Eccentricity: | 0.0030338 |
| inclination: | 100.1902° |
| perigee height: | 698 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 287.7514° |
| argument of perigee: | 319.5649° |
| revolutions per day: | 14.51705286 |
| mean anomaly at epoch: | 40.3285° |
| orbit number at epoch: | 4573 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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