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 12465U 81046B 24259.95377135 .00019738 00000-0 73059-3 0 9994
2 12465 81.2378 210.6825 0028697 83.9944 276.4560 15.27155411355636
| Epoch (UTC): | 15 September 2024 22:53:25 |
| Eccentricity: | 0.0028697 |
| inclination: | 81.2378° |
| perigee height: | 464 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 210.6825° |
| argument of perigee: | 83.9944° |
| revolutions per day: | 15.27155411 |
| mean anomaly at epoch: | 276.4560° |
| orbit number at epoch: | 35563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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