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 25544U 98067A 19201.54278260 .00016717 00000-0 10270-3 0 9037
2 25544 51.6376 195.7890 0006626 161.9077 198.2311 15.50996805 20421
| Epoch (UTC): | 20 July 2019 13:01:36 |
| Eccentricity: | 0.0006626 |
| inclination: | 51.6376° |
| perigee height: | 409 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 195.7890° |
| argument of perigee: | 161.9077° |
| revolutions per day: | 15.50996805 |
| mean anomaly at epoch: | 198.2311° |
| orbit number at epoch: | 2042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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