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 22148.81693703 .00002336 00000-0 12734-3 0 9992
2 20580 28.4703 298.9127 0002499 176.4028 330.8476 15.10520065563247
| Epoch (UTC): | 28 May 2022 19:36:23 |
| Eccentricity: | 0.0002499 |
| inclination: | 28.4703° |
| perigee height: | 533 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 298.9127° |
| argument of perigee: | 176.4028° |
| revolutions per day: | 15.10520065 |
| mean anomaly at epoch: | 330.8476° |
| orbit number at epoch: | 56324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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