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 24258.24390434 .00018489 00000-0 83837-3 0 9996
2 20580 28.4675 107.8107 0002469 305.9800 54.0564 15.19429093690843
| Epoch (UTC): | 14 September 2024 05:51:13 |
| Eccentricity: | 0.0002469 |
| inclination: | 28.4675° |
| perigee height: | 506 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 107.8107° |
| argument of perigee: | 305.9800° |
| revolutions per day: | 15.19429093 |
| mean anomaly at epoch: | 54.0564° |
| orbit number at epoch: | 69084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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