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 39120U 13011A 18271.83007568 0.00000000 00000-0 00000-0 0 00
2 39120 2.9394 326.9938 0001000 339.4665 20.5044 1.00270000 06
| Epoch (UTC): | 28 September 2018 19:55:18 |
| Eccentricity: | 0.0001000 |
| inclination: | 2.9394° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 326.9938° |
| argument of perigee: | 339.4665° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 20.5044° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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