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 39427U 26145.67203088 +.00000000 +00000-0 +19509-3 0 00007
2 39427 97.8258 55.9911 0088962 308.5177 50.8083 14.81595800 05
| Epoch (UTC): | 25 May 2026 16:07:43 |
| Eccentricity: | 0.0088962 |
| inclination: | 97.8258° |
| perigee height: | 562 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 55.9911° |
| argument of perigee: | 308.5177° |
| revolutions per day: | 14.81595800 |
| mean anomaly at epoch: | 50.8083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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