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 23090.87555080 .00012572 00000-0 13252-2 0 9998
2 39439 97.6734 58.7526 0058095 170.9116 189.3167 14.88202923505814
| Epoch (UTC): | 31 March 2023 21:00:47 |
| Eccentricity: | 0.0058095 |
| inclination: | 97.6734° |
| perigee height: | 563 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 58.7526° |
| argument of perigee: | 170.9116° |
| revolutions per day: | 14.88202923 |
| mean anomaly at epoch: | 189.3167° |
| orbit number at epoch: | 50581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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