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 25019U 97065A 18343.20506318 -.00000060 00000-0 00000+0 0 9994
2 25019 9.5647 39.8682 0008708 250.1719 109.6598 1.00273660 4067
| Epoch (UTC): | 09 December 2018 04:55:17 |
| Eccentricity: | 0.0008708 |
| inclination: | 9.5647° |
| perigee height: | 35749 km |
| apogee height: | 35822 km |
| right ascension of ascending node: | 39.8682° |
| argument of perigee: | 250.1719° |
| revolutions per day: | 1.00273660 |
| mean anomaly at epoch: | 109.6598° |
| orbit number at epoch: | 406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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