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 55474U 26145.33736975 +.00000000 +00000-0 +77078-4 0 00002
2 55474 42.9994 267.1933 0001252 251.3601 108.7115 15.27561914 07
| Epoch (UTC): | 25 May 2026 08:05:48 |
| Eccentricity: | 0.0001252 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 267.1933° |
| argument of perigee: | 251.3601° |
| revolutions per day: | 15.27561914 |
| mean anomaly at epoch: | 108.7115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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