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 18343.89983287 +.00000188 +00000-0 +62740-4 0 9997
2 26093 100.1978 209.8659 0030134 285.1900 074.5957 14.51514586993236
| Epoch (UTC): | 09 December 2018 21:35:45 |
| Eccentricity: | 0.0030134 |
| inclination: | 100.1978° |
| perigee height: | 699 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 209.8659° |
| argument of perigee: | 285.1900° |
| revolutions per day: | 14.51514586 |
| mean anomaly at epoch: | 74.5957° |
| orbit number at epoch: | 99323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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