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 20401U 90001A 18350.24830789 -.00000160 00000-0 00000+0 0 9992
2 20401 13.3799 7.8661 0017418 262.6501 268.6655 0.98999690101742
| Epoch (UTC): | 16 December 2018 05:57:33 |
| Eccentricity: | 0.0017418 |
| inclination: | 13.3799° |
| perigee height: | 36072 km |
| apogee height: | 36221 km |
| right ascension of ascending node: | 7.8661° |
| argument of perigee: | 262.6501° |
| revolutions per day: | 0.98999690 |
| mean anomaly at epoch: | 268.6655° |
| orbit number at epoch: | 10174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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