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 39439U 13066Z 23079.37690573 .00009419 00000-0 10031-2 0 9995
2 39439 97.6713 47.6224 0056964 209.3527 150.4487 14.87916360504100
| Epoch (UTC): | 20 March 2023 09:02:44 |
| Eccentricity: | 0.0056964 |
| inclination: | 97.6713° |
| perigee height: | 564 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 47.6224° |
| argument of perigee: | 209.3527° |
| revolutions per day: | 14.87916360 |
| mean anomaly at epoch: | 150.4487° |
| orbit number at epoch: | 50410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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