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 40100U 14043B 18295.35585775 0.00000000 00000-0 00000-0 0 00
2 40100 0.1686 160.1562 0006993 65.1101 294.9846 1.00541581 07
| Epoch (UTC): | 22 October 2018 08:32:26 |
| Eccentricity: | 0.0006993 |
| inclination: | 0.1686° |
| perigee height: | 35681 km |
| apogee height: | 35740 km |
| right ascension of ascending node: | 160.1562° |
| argument of perigee: | 65.1101° |
| revolutions per day: | 1.00541581 |
| mean anomaly at epoch: | 294.9846° |
| 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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