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 25226U 87068BD 24358.23106790 .00013938 00000-0 71715-2 0 9993
2 25226 82.5145 268.9419 0065921 348.7791 11.1911 14.14004641361734
| Epoch (UTC): | 23 December 2024 05:32:44 |
| Eccentricity: | 0.0065921 |
| inclination: | 82.5145° |
| perigee height: | 798 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 268.9419° |
| argument of perigee: | 348.7791° |
| revolutions per day: | 14.14004641 |
| mean anomaly at epoch: | 11.1911° |
| orbit number at epoch: | 36173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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