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 54695U 26145.64364355 +.00000000 +00000-0 +30746-3 0 00009
2 54695 97.6864 314.2098 0006444 185.8001 174.3168 15.34661696 06
| Epoch (UTC): | 25 May 2026 15:26:50 |
| Eccentricity: | 0.0006444 |
| inclination: | 97.6864° |
| perigee height: | 458 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 314.2098° |
| argument of perigee: | 185.8001° |
| revolutions per day: | 15.34661696 |
| mean anomaly at epoch: | 174.3168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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