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 35685U 09041E 19341.50707209 .00000104 00000-0 19338-4 0 9992
2 35685 98.2803 359.4714 0059042 12.5419 347.7247 14.84248102560250
| Epoch (UTC): | 07 December 2019 12:10:11 |
| Eccentricity: | 0.0059042 |
| inclination: | 98.2803° |
| perigee height: | 574 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 359.4714° |
| argument of perigee: | 12.5419° |
| revolutions per day: | 14.84248102 |
| mean anomaly at epoch: | 347.7247° |
| orbit number at epoch: | 56025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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