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 43472U 18045C 18140.97000001 -.00010094 +00000-0 +00000-0 0 9994
2 43472 027.5020 209.5210 9658153 171.2240 002.0960 00.09844104000019
| Epoch (UTC): | 20 May 2018 23:16:48 |
| Eccentricity: | 0.9658153 |
| inclination: | 27.5020° |
| perigee height: | 395 km |
| apogee height: | 383105 km |
| right ascension of ascending node: | 209.5210° |
| argument of perigee: | 171.2240° |
| revolutions per day: | 0.09844104 |
| mean anomaly at epoch: | 2.0960° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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