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 23033.47794781 .00004142 00000-0 22576-3 0 9998
2 20580 28.4708 83.4427 0002232 12.3774 117.1578 15.11818977601046
| Epoch (UTC): | 02 February 2023 11:28:14 |
| Eccentricity: | 0.0002232 |
| inclination: | 28.4708° |
| perigee height: | 529 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 83.4427° |
| argument of perigee: | 12.3774° |
| revolutions per day: | 15.11818977 |
| mean anomaly at epoch: | 117.1578° |
| orbit number at epoch: | 60104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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