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 23087.87075063 .00006255 00000-0 81831-3 0 9994
2 39440 97.7645 39.3181 0074502 289.0385 70.2767 14.78818483503489
| Epoch (UTC): | 28 March 2023 20:53:52 |
| Eccentricity: | 0.0074502 |
| inclination: | 97.7645° |
| perigee height: | 581 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 39.3181° |
| argument of perigee: | 289.0385° |
| revolutions per day: | 14.78818483 |
| mean anomaly at epoch: | 70.2767° |
| orbit number at epoch: | 50348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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