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 23332.92368883 .00008510 00000-0 43346-3 0 9991
2 20580 28.4687 250.5783 0002667 6.5721 61.1506 15.15020902646453
| Epoch (UTC): | 28 November 2023 22:10:06 |
| Eccentricity: | 0.0002667 |
| inclination: | 28.4687° |
| perigee height: | 519 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 250.5783° |
| argument of perigee: | 6.5721° |
| revolutions per day: | 15.15020902 |
| mean anomaly at epoch: | 61.1506° |
| orbit number at epoch: | 64645 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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