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 41558U 16033C 17229.38400741 .00001484 00000-0 58653-4 0 9992
2 41558 97.4635 308.9608 0014667 144.9286 215.2921 15.27025359 67768
| Epoch (UTC): | 17 August 2017 09:12:58 |
| Eccentricity: | 0.0014667 |
| inclination: | 97.4635° |
| perigee height: | 474 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 308.9608° |
| argument of perigee: | 144.9286° |
| revolutions per day: | 15.27025359 |
| mean anomaly at epoch: | 215.2921° |
| orbit number at epoch: | 6776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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