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 22221.20253565 .00001693 00000-0 88762-4 0 9995
2 20580 28.4689 179.2321 0002418 240.3773 140.8348 15.10738560574460
| Epoch (UTC): | 09 August 2022 04:51:39 |
| Eccentricity: | 0.0002418 |
| inclination: | 28.4689° |
| perigee height: | 532 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 179.2321° |
| argument of perigee: | 240.3773° |
| revolutions per day: | 15.10738560 |
| mean anomaly at epoch: | 140.8348° |
| orbit number at epoch: | 57446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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