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 20580U 90037B 19264.24123087 .00000393 00000-0 12974-4 0 9995
2 20580 28.4698 306.7166 0002935 64.4283 355.8712 15.09268348415185
| Epoch (UTC): | 21 September 2019 05:47:22 |
| Eccentricity: | 0.0002935 |
| inclination: | 28.4698° |
| perigee height: | 536 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 306.7166° |
| argument of perigee: | 64.4283° |
| revolutions per day: | 15.09268348 |
| mean anomaly at epoch: | 355.8712° |
| orbit number at epoch: | 41518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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