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 42932U 17052A 19040.23716514 0.00000200 00000-0 13060-5 0 08
2 42932 54.5148 116.9172 0002500 95.0039 264.9960 15.75203796 00
| Epoch (UTC): | 09 February 2019 05:41:31 |
| Eccentricity: | 0.0002500 |
| inclination: | 54.5148° |
| perigee height: | 342 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 116.9172° |
| argument of perigee: | 95.0039° |
| revolutions per day: | 15.75203796 |
| mean anomaly at epoch: | 264.9960° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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