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 39234U 26145.52709845 +.00000000 +00000-0 +00000-0 0 00002
2 39234 0.0929 92.5882 0003469 205.1230 209.1657 1.00271585 01
| Epoch (UTC): | 25 May 2026 12:39:01 |
| Eccentricity: | 0.0003469 |
| inclination: | 0.0929° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 92.5882° |
| argument of perigee: | 205.1230° |
| revolutions per day: | 1.00271585 |
| mean anomaly at epoch: | 209.1657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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