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 39188U 26145.45239043 +.00000000 +00000-0 +00000-0 0 00000
2 39188 0.1006 351.4325 0003036 60.0086 308.5858 5.00116533 04
| Epoch (UTC): | 25 May 2026 10:51:26 |
| Eccentricity: | 0.0003036 |
| inclination: | 0.1006° |
| perigee height: | 8061 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 351.4325° |
| argument of perigee: | 60.0086° |
| revolutions per day: | 5.00116533 |
| mean anomaly at epoch: | 308.5858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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