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 55175U 26145.38142876 +.00000000 +00000-0 -13244-2 0 00000
2 55175 87.8911 25.6053 0002054 90.7494 269.3869 13.11416068 08
| Epoch (UTC): | 25 May 2026 09:09:15 |
| Eccentricity: | 0.0002054 |
| inclination: | 87.8911° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6053° |
| argument of perigee: | 90.7494° |
| revolutions per day: | 13.11416068 |
| mean anomaly at epoch: | 269.3869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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