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 55148U 26145.23100644 +.00000000 +00000-0 -52845-3 0 00002
2 55148 87.8948 324.7914 0000894 88.3806 271.7426 13.13468708 03
| Epoch (UTC): | 25 May 2026 05:32:38 |
| Eccentricity: | 0.0000894 |
| inclination: | 87.8948° |
| perigee height: | 1209 km |
| apogee height: | 1210 km |
| right ascension of ascending node: | 324.7914° |
| argument of perigee: | 88.3806° |
| revolutions per day: | 13.13468708 |
| mean anomaly at epoch: | 271.7426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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