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 26064U 00004D 24285.46217114 .00001090 00000-0 38541-3 0 9993
2 26064 100.2263 90.5462 0037184 350.7654 9.2839 14.36883028294855
| Epoch (UTC): | 11 October 2024 11:05:31 |
| Eccentricity: | 0.0037184 |
| inclination: | 100.2263° |
| perigee height: | 742 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 90.5462° |
| argument of perigee: | 350.7654° |
| revolutions per day: | 14.36883028 |
| mean anomaly at epoch: | 9.2839° |
| orbit number at epoch: | 29485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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