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 23086.74724642 .00005771 00000-0 31245-3 0 9997
2 20580 28.4697 89.6090 0002651 213.5704 316.4145 15.12505681609116
| Epoch (UTC): | 27 March 2023 17:56:02 |
| Eccentricity: | 0.0002651 |
| inclination: | 28.4697° |
| perigee height: | 527 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 89.6090° |
| argument of perigee: | 213.5704° |
| revolutions per day: | 15.12505681 |
| mean anomaly at epoch: | 316.4145° |
| orbit number at epoch: | 60911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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