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 28158U 04004A 18184.09704861 0.00000000 00000-0 00000-0 0 02
2 28158 8.3360 43.6780 0001540 71.8490 287.6678 1.00270000 07
| Epoch (UTC): | 03 July 2018 02:19:45 |
| Eccentricity: | 0.0001540 |
| inclination: | 8.3360° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 43.6780° |
| argument of perigee: | 71.8490° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 287.6678° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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