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 39770U 14029E 19258.76926159 .00000416 00000-0 52069-4 0 9999
2 39770 97.8862 1.5023 0009192 146.3507 213.8287 14.87417675288072
| Epoch (UTC): | 15 September 2019 18:27:44 |
| Eccentricity: | 0.0009192 |
| inclination: | 97.8862° |
| perigee height: | 599 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 1.5023° |
| argument of perigee: | 146.3507° |
| revolutions per day: | 14.87417675 |
| mean anomaly at epoch: | 213.8287° |
| orbit number at epoch: | 28807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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