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 39483U 13076A 18146.73535310 .00000021 00000-0 77232-4 0 9999
2 39483 82.4849 203.0534 0020433 35.5381 324.7055 12.42886058200437
| Epoch (UTC): | 26 May 2018 17:38:54 |
| Eccentricity: | 0.0020433 |
| inclination: | 82.4849° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 203.0534° |
| argument of perigee: | 35.5381° |
| revolutions per day: | 12.42886058 |
| mean anomaly at epoch: | 324.7055° |
| orbit number at epoch: | 20043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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