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 39191U 26145.45153411 +.00000000 +00000-0 +00000-0 0 00008
2 39191 0.0690 356.3686 0005387 66.7312 296.9549 5.00116036 01
| Epoch (UTC): | 25 May 2026 10:50:12 |
| Eccentricity: | 0.0005387 |
| inclination: | 0.0690° |
| perigee height: | 8058 km |
| apogee height: | 8074 km |
| right ascension of ascending node: | 356.3686° |
| argument of perigee: | 66.7312° |
| revolutions per day: | 5.00116036 |
| mean anomaly at epoch: | 296.9549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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