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 05435U 71071A 18176.06368511 -.00000109 00000-0 20145-4 0 9993
2 05435 50.1421 7.2199 0110570 20.4821 340.0490 14.55112926471896
| Epoch (UTC): | 25 June 2018 01:31:42 |
| Eccentricity: | 0.0110570 |
| inclination: | 50.1421° |
| perigee height: | 630 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 7.2199° |
| argument of perigee: | 20.4821° |
| revolutions per day: | 14.55112926 |
| mean anomaly at epoch: | 340.0490° |
| orbit number at epoch: | 47189 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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