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 18267.64054456 +.00001298 +00000-0 +56142-4 0 9998
2 42015 097.4384 331.7898 0007471 041.9486 318.2322 15.24232257089066
| Epoch (UTC): | 24 September 2018 15:22:23 |
| Eccentricity: | 0.0007471 |
| inclination: | 97.4384° |
| perigee height: | 488 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 331.7898° |
| argument of perigee: | 41.9486° |
| revolutions per day: | 15.24232257 |
| mean anomaly at epoch: | 318.2322° |
| orbit number at epoch: | 8906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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