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 18347.85821404 +.00001023 +00000-0 +44616-4 0 9994
2 42015 097.4273 051.3376 0008107 105.1356 255.0779 15.24428387101289
| Epoch (UTC): | 13 December 2018 20:35:49 |
| Eccentricity: | 0.0008107 |
| inclination: | 97.4273° |
| perigee height: | 487 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 51.3376° |
| argument of perigee: | 105.1356° |
| revolutions per day: | 15.24428387 |
| mean anomaly at epoch: | 255.0779° |
| orbit number at epoch: | 10128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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