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 27436U 02026A 18114.78537809 +.00000027 +00000-0 +12400-4 0 9994
2 27436 082.9538 210.6490 0044960 281.8158 192.0063 13.74924538798233
| Epoch (UTC): | 24 April 2018 18:50:56 |
| Eccentricity: | 0.0044960 |
| inclination: | 82.9538° |
| perigee height: | 949 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 210.6490° |
| argument of perigee: | 281.8158° |
| revolutions per day: | 13.74924538 |
| mean anomaly at epoch: | 192.0063° |
| orbit number at epoch: | 79823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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