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 23267.56573062 .00006488 00000-0 33663-3 0 9998
2 20580 28.4705 326.3448 0002365 26.2288 86.9044 15.14131942636532
| Epoch (UTC): | 24 September 2023 13:34:39 |
| Eccentricity: | 0.0002365 |
| inclination: | 28.4705° |
| perigee height: | 522 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 326.3448° |
| argument of perigee: | 26.2288° |
| revolutions per day: | 15.14131942 |
| mean anomaly at epoch: | 86.9044° |
| orbit number at epoch: | 63653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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