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 23036.45059442 .00003961 00000-0 21527-3 0 9990
2 20580 28.4707 63.7083 0002417 43.4972 97.0532 15.11840398601491
| Epoch (UTC): | 05 February 2023 10:48:51 |
| Eccentricity: | 0.0002417 |
| inclination: | 28.4707° |
| perigee height: | 529 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 63.7083° |
| argument of perigee: | 43.4972° |
| revolutions per day: | 15.11840398 |
| mean anomaly at epoch: | 97.0532° |
| orbit number at epoch: | 60149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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