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 19419U 88074A 18344.16835431 .00000061 00000-0 89838-4 0 9999
2 19419 89.9890 18.3041 0095894 346.9416 75.2113 13.42201302483297
| Epoch (UTC): | 10 December 2018 04:02:25 |
| Eccentricity: | 0.0095894 |
| inclination: | 89.9890° |
| perigee height: | 1029 km |
| apogee height: | 1173 km |
| right ascension of ascending node: | 18.3041° |
| argument of perigee: | 346.9416° |
| revolutions per day: | 13.42201302 |
| mean anomaly at epoch: | 75.2113° |
| orbit number at epoch: | 48329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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