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 35938U 09052B 19103.81683765 0.00000000 00000-0 00000-0 0 05
2 35938 57.9917 24.0811 0010201 253.6595 106.3405 12.79305868 01
| Epoch (UTC): | 13 April 2019 19:36:14 |
| Eccentricity: | 0.0010201 |
| inclination: | 57.9917° |
| perigee height: | 1336 km |
| apogee height: | 1352 km |
| right ascension of ascending node: | 24.0811° |
| argument of perigee: | 253.6595° |
| revolutions per day: | 12.79305868 |
| mean anomaly at epoch: | 106.3405° |
| 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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