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 27540U 02048A 18117.68325543 .00000532 00000-0 00000+0 0 9995
2 27540 48.8690 171.5266 8484026 267.1663 0.1656 0.37594331 15487
| Epoch (UTC): | 27 April 2018 16:23:53 |
| Eccentricity: | 0.8484026 |
| inclination: | 48.8690° |
| perigee height: | 5915 km |
| apogee height: | 143514 km |
| right ascension of ascending node: | 171.5266° |
| argument of perigee: | 267.1663° |
| revolutions per day: | 0.37594331 |
| mean anomaly at epoch: | 0.1656° |
| orbit number at epoch: | 1548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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