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 39416U 13066A 19077.52988058 .00000089 00000-0 16855-4 0 9994
2 39416 97.5543 106.5367 0040014 310.9586 48.8169 14.83868768288033
| Epoch (UTC): | 18 March 2019 12:43:01 |
| Eccentricity: | 0.0040014 |
| inclination: | 97.5543° |
| perigee height: | 589 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 106.5367° |
| argument of perigee: | 310.9586° |
| revolutions per day: | 14.83868768 |
| mean anomaly at epoch: | 48.8169° |
| orbit number at epoch: | 28803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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