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 23335.11081230 .00007883 00000-0 40040-3 0 9993
2 20580 28.4678 235.9859 0002699 29.4466 110.9157 15.15055834647053
| Epoch (UTC): | 01 December 2023 02:39:34 |
| Eccentricity: | 0.0002699 |
| inclination: | 28.4678° |
| perigee height: | 519 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 235.9859° |
| argument of perigee: | 29.4466° |
| revolutions per day: | 15.15055834 |
| mean anomaly at epoch: | 110.9157° |
| orbit number at epoch: | 64705 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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