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 55048U 26145.60625036 +.00000000 +00000-0 +39119-3 0 00007
2 55048 97.1873 198.9192 0011907 173.2061 186.9347 15.34447472 05
| Epoch (UTC): | 25 May 2026 14:33:00 |
| Eccentricity: | 0.0011907 |
| inclination: | 97.1873° |
| perigee height: | 454 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 198.9192° |
| argument of perigee: | 173.2061° |
| revolutions per day: | 15.34447472 |
| mean anomaly at epoch: | 186.9347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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