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 23081.44262792 .00005941 00000-0 77879-3 0 9996
2 39440 97.7645 33.1134 0074960 310.3792 49.0892 14.78728972502538
| Epoch (UTC): | 22 March 2023 10:37:23 |
| Eccentricity: | 0.0074960 |
| inclination: | 97.7645° |
| perigee height: | 581 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 33.1134° |
| argument of perigee: | 310.3792° |
| revolutions per day: | 14.78728972 |
| mean anomaly at epoch: | 49.0892° |
| orbit number at epoch: | 50253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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