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 39444U 13066AE 23265.89218742 .00008033 00000-0 86660-3 0 9992
2 39444 97.6816 226.8727 0050662 311.9912 47.6995 14.87699159530166
| Epoch (UTC): | 22 September 2023 21:24:44 |
| Eccentricity: | 0.0050662 |
| inclination: | 97.6816° |
| perigee height: | 570 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 226.8727° |
| argument of perigee: | 311.9912° |
| revolutions per day: | 14.87699159 |
| mean anomaly at epoch: | 47.6995° |
| orbit number at epoch: | 53016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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