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 42015U 17008BV 19077.63690292 +.00001342 +00000-0 +57267-4 0 9990
2 42015 097.4120 145.2018 0007792 126.2798 233.9160 15.24631814115723
| Epoch (UTC): | 18 March 2019 15:17:08 |
| Eccentricity: | 0.0007792 |
| inclination: | 97.4120° |
| perigee height: | 486 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 145.2018° |
| argument of perigee: | 126.2798° |
| revolutions per day: | 15.24631814 |
| mean anomaly at epoch: | 233.9160° |
| orbit number at epoch: | 11572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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