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 23157.57679965 .00004177 00000-0 21902-3 0 9992
2 20580 28.4708 338.6021 0002120 266.1979 156.6746 15.13194023619857
| Epoch (UTC): | 06 June 2023 13:50:35 |
| Eccentricity: | 0.0002120 |
| inclination: | 28.4708° |
| perigee height: | 525 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 338.6021° |
| argument of perigee: | 266.1979° |
| revolutions per day: | 15.13194023 |
| mean anomaly at epoch: | 156.6746° |
| orbit number at epoch: | 61985 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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