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 26145.35856674 +.00000000 +00000-0 +90166-4 0 00002
2 39423 97.7175 296.1387 0161914 304.0961 54.4964 14.58027619 05
| Epoch (UTC): | 25 May 2026 08:36:20 |
| Eccentricity: | 0.0161914 |
| inclination: | 97.7175° |
| perigee height: | 585 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 296.1387° |
| argument of perigee: | 304.0961° |
| revolutions per day: | 14.58027619 |
| mean anomaly at epoch: | 54.4964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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