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 39423U 26145.15268801 +.00000000 +00000-0 +89963-4 0 00002
2 39423 97.7175 295.9475 0161921 304.7485 53.8559 14.58027413 01
| Epoch (UTC): | 25 May 2026 03:39:52 |
| Eccentricity: | 0.0161921 |
| inclination: | 97.7175° |
| perigee height: | 585 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 295.9475° |
| argument of perigee: | 304.7485° |
| revolutions per day: | 14.58027413 |
| mean anomaly at epoch: | 53.8559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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