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 39485U 13076C 19016.73144265 .00000022 00000-0 85863-4 0 9993
2 39485 82.4817 56.4211 0020157 253.2159 106.6706 12.42895490229634
| Epoch (UTC): | 16 January 2019 17:33:16 |
| Eccentricity: | 0.0020157 |
| inclination: | 82.4817° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 56.4211° |
| argument of perigee: | 253.2159° |
| revolutions per day: | 12.42895490 |
| mean anomaly at epoch: | 106.6706° |
| orbit number at epoch: | 22963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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