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 34690U 97051KM 24357.84197980 .00005403 00000-0 13316-2 0 9999
2 34690 86.3829 190.8422 0012013 121.8867 301.0613 14.52007001829380
| Epoch (UTC): | 22 December 2024 20:12:27 |
| Eccentricity: | 0.0012013 |
| inclination: | 86.3829° |
| perigee height: | 710 km |
| apogee height: | 727 km |
| right ascension of ascending node: | 190.8422° |
| argument of perigee: | 121.8867° |
| revolutions per day: | 14.52007001 |
| mean anomaly at epoch: | 301.0613° |
| orbit number at epoch: | 82938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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