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 23340.04729344 .00005011 00000-0 25049-3 0 9999
2 20580 28.4675 203.0446 0002803 78.4367 40.8361 15.15123365647535
| Epoch (UTC): | 06 December 2023 01:08:06 |
| Eccentricity: | 0.0002803 |
| inclination: | 28.4675° |
| perigee height: | 518 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 203.0446° |
| argument of perigee: | 78.4367° |
| revolutions per day: | 15.15123365 |
| mean anomaly at epoch: | 40.8361° |
| orbit number at epoch: | 64753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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