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 39136U 13015G 18139.76204960 .00000908 00000-0 56847-4 0 9999
2 39136 64.8694 234.5517 0023236 238.9676 120.9168 15.16101389280287
| Epoch (UTC): | 19 May 2018 18:17:21 |
| Eccentricity: | 0.0023236 |
| inclination: | 64.8694° |
| perigee height: | 501 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 234.5517° |
| argument of perigee: | 238.9676° |
| revolutions per day: | 15.16101389 |
| mean anomaly at epoch: | 120.9168° |
| orbit number at epoch: | 28028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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