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 57238U 26145.49650679 +.00000000 +00000-0 +76028-5 0 00000
2 57238 43.0056 306.3762 0001571 269.7165 90.3507 15.27575101 00
| Epoch (UTC): | 25 May 2026 11:54:58 |
| Eccentricity: | 0.0001571 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.3762° |
| argument of perigee: | 269.7165° |
| revolutions per day: | 15.27575101 |
| mean anomaly at epoch: | 90.3507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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