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 23334.82524645 .00000692 00000-0 29376-3 0 9997
2 26931 67.0499 126.5119 0005794 258.3420 101.7032 14.31057012157586
| Epoch (UTC): | 30 November 2023 19:48:21 |
| Eccentricity: | 0.0005794 |
| inclination: | 67.0499° |
| perigee height: | 784 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 126.5119° |
| argument of perigee: | 258.3420° |
| revolutions per day: | 14.31057012 |
| mean anomaly at epoch: | 101.7032° |
| orbit number at epoch: | 15758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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