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 23967U 96042A 23266.62274299 .00000056 00000-0 00000+0 0 9998
2 23967 10.1858 21.7754 0008413 99.9638 288.1595 1.00280104 99493
| Epoch (UTC): | 23 September 2023 14:56:44 |
| Eccentricity: | 0.0008413 |
| inclination: | 10.1858° |
| perigee height: | 35748 km |
| apogee height: | 35819 km |
| right ascension of ascending node: | 21.7754° |
| argument of perigee: | 99.9638° |
| revolutions per day: | 1.00280104 |
| mean anomaly at epoch: | 288.1595° |
| orbit number at epoch: | 9949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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