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 26931U 01043C 23333.77690659 .00000602 00000-0 25955-3 0 9999
2 26931 67.0497 129.2193 0005824 257.9957 102.0492 14.31055080157431
| Epoch (UTC): | 29 November 2023 18:38:44 |
| Eccentricity: | 0.0005824 |
| inclination: | 67.0497° |
| perigee height: | 784 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 129.2193° |
| argument of perigee: | 257.9957° |
| revolutions per day: | 14.31055080 |
| mean anomaly at epoch: | 102.0492° |
| orbit number at epoch: | 15743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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