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 39472U 26145.26817498 +.00000000 +00000-0 +14481-2 0 00001
2 39472 120.4725 66.9049 0043290 39.3081 321.1153 15.82327902 09
| Epoch (UTC): | 25 May 2026 06:26:10 |
| Eccentricity: | 0.0043290 |
| inclination: | 120.4725° |
| perigee height: | 295 km |
| apogee height: | 353 km |
| right ascension of ascending node: | 66.9049° |
| argument of perigee: | 39.3081° |
| revolutions per day: | 15.82327902 |
| mean anomaly at epoch: | 321.1153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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