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 24944U 26017.81368845 +.00000000 +00000-0 +98254-4 0 00007
2 24944 86.3919 53.7891 0002058 89.4153 270.7280 14.36692749 06
| Epoch (UTC): | 17 January 2026 19:31:42 |
| Eccentricity: | 0.0002058 |
| inclination: | 86.3919° |
| perigee height: | 768 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 53.7891° |
| argument of perigee: | 89.4153° |
| revolutions per day: | 14.36692749 |
| mean anomaly at epoch: | 270.7280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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