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 23338.52937240 .00000507 00000-0 22382-3 0 9992
2 26931 67.0503 116.9449 0005698 258.4015 101.6447 14.31060926157953
| Epoch (UTC): | 04 December 2023 12:42:17 |
| Eccentricity: | 0.0005698 |
| inclination: | 67.0503° |
| perigee height: | 784 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 116.9449° |
| argument of perigee: | 258.4015° |
| revolutions per day: | 14.31060926 |
| mean anomaly at epoch: | 101.6447° |
| orbit number at epoch: | 15795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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