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 18094.89502497 0.00000000 00000-0 00000-0 0 06
2 40100 0.0230 84.4230 0000750 211.5960 148.4040 1.00501339 02
| Epoch (UTC): | 04 April 2018 21:28:50 |
| Eccentricity: | 0.0000750 |
| inclination: | 0.0230° |
| perigee height: | 35719 km |
| apogee height: | 35725 km |
| right ascension of ascending node: | 84.4230° |
| argument of perigee: | 211.5960° |
| revolutions per day: | 1.00501339 |
| mean anomaly at epoch: | 148.4040° |
| 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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