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 39440U 13066AA 23086.85580633 .00005607 00000-0 73448-3 0 9990
2 39440 97.7645 38.3384 0074527 292.4145 66.9184 14.78805895502131
| Epoch (UTC): | 27 March 2023 20:32:21 |
| Eccentricity: | 0.0074527 |
| inclination: | 97.7645° |
| perigee height: | 581 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 38.3384° |
| argument of perigee: | 292.4145° |
| revolutions per day: | 14.78805895 |
| mean anomaly at epoch: | 66.9184° |
| orbit number at epoch: | 50213 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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