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 39485U 13076C 23083.81041829 -.00002236 00000-0 -16213-1 0 9994
2 39485 82.4877 183.8981 0021774 161.7299 198.4444 12.42865814419460
| Epoch (UTC): | 24 March 2023 19:27:00 |
| Eccentricity: | 0.0021774 |
| inclination: | 82.4877° |
| perigee height: | 1477 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 183.8981° |
| argument of perigee: | 161.7299° |
| revolutions per day: | 12.42865814 |
| mean anomaly at epoch: | 198.4444° |
| orbit number at epoch: | 41946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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