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 43628U 13065E 24355.07653202 .00021509 00000-0 67886-2 0 9996
2 43628 100.5293 209.7169 0168761 239.7076 118.7310 14.32420827325714
| Epoch (UTC): | 20 December 2024 01:50:12 |
| Eccentricity: | 0.0168761 |
| inclination: | 100.5293° |
| perigee height: | 663 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 209.7169° |
| argument of perigee: | 239.7076° |
| revolutions per day: | 14.32420827 |
| mean anomaly at epoch: | 118.7310° |
| orbit number at epoch: | 32571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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