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 57406U 26145.49708141 +.00000000 +00000-0 +52366-4 0 00003
2 57406 43.0036 181.9023 0001680 279.3110 80.7551 15.26743313 03
| Epoch (UTC): | 25 May 2026 11:55:47 |
| Eccentricity: | 0.0001680 |
| inclination: | 43.0036° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 181.9023° |
| argument of perigee: | 279.3110° |
| revolutions per day: | 15.26743313 |
| mean anomaly at epoch: | 80.7551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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