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 12175U 26017.94234155 +.00000000 +00000-0 +88154-4 0 00008
2 12175 99.2323 272.0923 0063441 99.1485 277.9231 13.97309973 07
| Epoch (UTC): | 17 January 2026 22:36:58 |
| Eccentricity: | 0.0063441 |
| inclination: | 99.2323° |
| perigee height: | 857 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 272.0923° |
| argument of perigee: | 99.1485° |
| revolutions per day: | 13.97309973 |
| mean anomaly at epoch: | 277.9231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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