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 20547U 90028B 23088.38389613 .00006003 00000-0 20300-3 0 9996
2 20547 94.1023 208.0787 0074696 284.5966 74.7006 15.28033301821442
| Epoch (UTC): | 29 March 2023 09:12:48 |
| Eccentricity: | 0.0074696 |
| inclination: | 94.1023° |
| perigee height: | 430 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 208.0787° |
| argument of perigee: | 284.5966° |
| revolutions per day: | 15.28033301 |
| mean anomaly at epoch: | 74.7006° |
| orbit number at epoch: | 82144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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