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 57239U 26144.89758772 +.00000000 +00000-0 +53477-4 0 00009
2 57239 43.0047 320.0603 0002002 273.4106 86.6517 15.27580355 01
| Epoch (UTC): | 24 May 2026 21:32:31 |
| Eccentricity: | 0.0002002 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.0603° |
| argument of perigee: | 273.4106° |
| revolutions per day: | 15.27580355 |
| mean anomaly at epoch: | 86.6517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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