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 is defined by the following mean orbital elements,
1 25979U 26024.17587013 +.00000000 +00000-0 +10740-2 0 00005
2 25979 98.1714 101.8589 0003791 232.6547 127.4346 15.29444673 07
| Epoch (UTC): | 24 January 2026 04:13:15 |
| Eccentricity: | 0.0003791 |
| inclination: | 98.1714° |
| perigee height: | 475 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 101.8589° |
| argument of perigee: | 232.6547° |
| revolutions per day: | 15.29444673 |
| mean anomaly at epoch: | 127.4346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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