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 39433U 13066T 23081.48744620 .00013441 00000-0 11419-2 0 9998
2 39433 97.4529 84.2095 0028562 29.2012 331.0801 14.97670458507950
| Epoch (UTC): | 22 March 2023 11:41:55 |
| Eccentricity: | 0.0028562 |
| inclination: | 97.4529° |
| perigee height: | 554 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 84.2095° |
| argument of perigee: | 29.2012° |
| revolutions per day: | 14.97670458 |
| mean anomaly at epoch: | 331.0801° |
| orbit number at epoch: | 50795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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