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 26474U 00047B 23265.82042499 .00004080 00000-0 33112-3 0 9995
2 26474 67.9953 28.6952 0054654 320.7214 38.9970 14.99530120257698
| Epoch (UTC): | 22 September 2023 19:41:24 |
| Eccentricity: | 0.0054654 |
| inclination: | 67.9953° |
| perigee height: | 530 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 28.6952° |
| argument of perigee: | 320.7214° |
| revolutions per day: | 14.99530120 |
| mean anomaly at epoch: | 38.9970° |
| orbit number at epoch: | 25769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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