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 22140.29683640 .00003901 00000-0 22025-3 0 9998
2 20580 28.4712 355.3605 0002865 90.3933 74.4422 15.10466071561956
| Epoch (UTC): | 20 May 2022 07:07:26 |
| Eccentricity: | 0.0002865 |
| inclination: | 28.4712° |
| perigee height: | 533 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 355.3605° |
| argument of perigee: | 90.3933° |
| revolutions per day: | 15.10466071 |
| mean anomaly at epoch: | 74.4422° |
| orbit number at epoch: | 56195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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