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 55675U 26145.22562522 +.00000000 +00000-0 +19102-4 0 00002
2 55675 69.9989 331.2895 0002874 269.5550 90.5279 14.98330867 05
| Epoch (UTC): | 25 May 2026 05:24:54 |
| Eccentricity: | 0.0002874 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.2895° |
| argument of perigee: | 269.5550° |
| revolutions per day: | 14.98330867 |
| mean anomaly at epoch: | 90.5279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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