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 7648U 75011A 23344.61091920 .00000129 00000-0 00000+0 0 9994
2 7648 7.7790 293.4567 0013669 247.5069 349.2644 0.99507823126588
| Epoch (UTC): | 10 December 2023 14:39:43 |
| Eccentricity: | 0.0013669 |
| inclination: | 7.7790° |
| perigee height: | 35944 km |
| apogee height: | 36059 km |
| right ascension of ascending node: | 293.4567° |
| argument of perigee: | 247.5069° |
| revolutions per day: | 0.99507823 |
| mean anomaly at epoch: | 349.2644° |
| orbit number at epoch: | 12658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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