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 40028U 14033U 18175.80856986 .00000391 00000-0 47999-4 0 9992
2 40028 97.9097 91.5868 0013988 152.8224 207.3740 14.88580145217903
| Epoch (UTC): | 24 June 2018 19:24:20 |
| Eccentricity: | 0.0013988 |
| inclination: | 97.9097° |
| perigee height: | 592 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 91.5868° |
| argument of perigee: | 152.8224° |
| revolutions per day: | 14.88580145 |
| mean anomaly at epoch: | 207.3740° |
| orbit number at epoch: | 21790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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