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 18171.12971213 .00001112 00000-0 48852-4 0 9998
2 42015 97.4473 235.9634 0007016 23.9308 336.2254 15.24016378 74361
| Epoch (UTC): | 20 June 2018 03:06:47 |
| Eccentricity: | 0.0007016 |
| inclination: | 97.4473° |
| perigee height: | 489 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 235.9634° |
| argument of perigee: | 23.9308° |
| revolutions per day: | 15.24016378 |
| mean anomaly at epoch: | 336.2254° |
| orbit number at epoch: | 7436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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