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 23270.53330274 .00006746 00000-0 35000-3 0 9999
2 20580 28.4698 306.5732 0002556 55.7567 65.6771 15.14175293636985
| Epoch (UTC): | 27 September 2023 12:47:57 |
| Eccentricity: | 0.0002556 |
| inclination: | 28.4698° |
| perigee height: | 522 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 306.5732° |
| argument of perigee: | 55.7567° |
| revolutions per day: | 15.14175293 |
| mean anomaly at epoch: | 65.6771° |
| orbit number at epoch: | 63698 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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