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 22180.46872187 .00001300 00000-0 65853-4 0 9995
2 20580 28.4701 89.1828 0002616 161.7017 10.9772 15.10615879568034
| Epoch (UTC): | 29 June 2022 11:14:57 |
| Eccentricity: | 0.0002616 |
| inclination: | 28.4701° |
| perigee height: | 532 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 89.1828° |
| argument of perigee: | 161.7017° |
| revolutions per day: | 15.10615879 |
| mean anomaly at epoch: | 10.9772° |
| orbit number at epoch: | 56803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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