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 31128U 07012M 23083.29569227 .00007849 00000-0 16315-2 0 9999
2 31128 98.2956 25.5443 0094877 150.6941 209.9626 14.57527053845954
| Epoch (UTC): | 24 March 2023 07:05:47 |
| Eccentricity: | 0.0094877 |
| inclination: | 98.2956° |
| perigee height: | 634 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 25.5443° |
| argument of perigee: | 150.6941° |
| revolutions per day: | 14.57527053 |
| mean anomaly at epoch: | 209.9626° |
| orbit number at epoch: | 84595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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