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 22269.11087751 .00002405 00000-0 12995-3 0 9995
2 20580 28.4695 221.6643 0002590 45.5140 63.8437 15.10916028581457
| Epoch (UTC): | 26 September 2022 02:39:39 |
| Eccentricity: | 0.0002590 |
| inclination: | 28.4695° |
| perigee height: | 531 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 221.6643° |
| argument of perigee: | 45.5140° |
| revolutions per day: | 15.10916028 |
| mean anomaly at epoch: | 63.8437° |
| orbit number at epoch: | 58145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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