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 25520U 98064B 19082.93244970 +.00000633 +00000-0 +14065-4 0 9991
2 25520 028.4514 270.3632 0004927 320.0051 040.0181 15.29083884132745
| Epoch (UTC): | 23 March 2019 22:22:43 |
| Eccentricity: | 0.0004927 |
| inclination: | 28.4514° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 270.3632° |
| argument of perigee: | 320.0051° |
| revolutions per day: | 15.29083884 |
| mean anomaly at epoch: | 40.0181° |
| orbit number at epoch: | 13274 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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