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 24357.52978924 .00000377 00000-0 14584-3 0 9991
2 26064 100.2260 176.0635 0037604 145.8468 214.5143 14.36980567304966
| Epoch (UTC): | 22 December 2024 12:42:53 |
| Eccentricity: | 0.0037604 |
| inclination: | 100.2260° |
| perigee height: | 741 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 176.0635° |
| argument of perigee: | 145.8468° |
| revolutions per day: | 14.36980567 |
| mean anomaly at epoch: | 214.5143° |
| orbit number at epoch: | 30496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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