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 35868U 09049D 19081.94266117 +.00000004 +00000-0 +20145-4 0 9997
2 35868 098.4006 085.7129 0005193 057.3554 302.8125 14.22842942493698
| Epoch (UTC): | 22 March 2019 22:37:25 |
| Eccentricity: | 0.0005193 |
| inclination: | 98.4006° |
| perigee height: | 812 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 85.7129° |
| argument of perigee: | 57.3554° |
| revolutions per day: | 14.22842942 |
| mean anomaly at epoch: | 302.8125° |
| orbit number at epoch: | 49369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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