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 28909U 05048B 19016.71543972 .00000072 00000-0 37920-3 0 9993
2 28909 82.4678 241.1114 0007781 82.2317 277.9653 12.55177932598873
| Epoch (UTC): | 16 January 2019 17:10:13 |
| Eccentricity: | 0.0007781 |
| inclination: | 82.4678° |
| perigee height: | 1437 km |
| apogee height: | 1449 km |
| right ascension of ascending node: | 241.1114° |
| argument of perigee: | 82.2317° |
| revolutions per day: | 12.55177932 |
| mean anomaly at epoch: | 277.9653° |
| orbit number at epoch: | 59887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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