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 18078.43099537 0.00000000 00000-0 00000-0 0 09
2 28158 8.0790 44.4000 0001410 330.3680 29.1241 1.00410105 02
| Epoch (UTC): | 19 March 2018 10:20:38 |
| Eccentricity: | 0.0001410 |
| inclination: | 8.0790° |
| perigee height: | 35741 km |
| apogee height: | 35753 km |
| right ascension of ascending node: | 44.4000° |
| argument of perigee: | 330.3680° |
| revolutions per day: | 1.00410105 |
| mean anomaly at epoch: | 29.1241° |
| 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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