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 39422U 26145.60555045 +.00000000 +00000-0 +17711-3 0 00001
2 39422 97.6163 115.8653 0010397 107.7519 252.4841 15.02579403 05
| Epoch (UTC): | 25 May 2026 14:31:59 |
| Eccentricity: | 0.0010397 |
| inclination: | 97.6163° |
| perigee height: | 552 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 115.8653° |
| argument of perigee: | 107.7519° |
| revolutions per day: | 15.02579403 |
| mean anomaly at epoch: | 252.4841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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