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 42000U 17008BE 19054.43416742 .00000811 00000-0 36740-4 0 9996
2 42000 97.4158 121.4533 0007962 199.2516 160.8421 15.23673255111653
| Epoch (UTC): | 23 February 2019 10:25:12 |
| Eccentricity: | 0.0007962 |
| inclination: | 97.4158° |
| perigee height: | 489 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 121.4533° |
| argument of perigee: | 199.2516° |
| revolutions per day: | 15.23673255 |
| mean anomaly at epoch: | 160.8421° |
| orbit number at epoch: | 11165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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