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 57246U 26144.85405647 +.00000000 +00000-0 +35752-4 0 00009
2 57246 43.0033 309.2981 0001498 263.9219 96.1462 15.27581861 07
| Epoch (UTC): | 24 May 2026 20:29:50 |
| Eccentricity: | 0.0001498 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.2981° |
| argument of perigee: | 263.9219° |
| revolutions per day: | 15.27581861 |
| mean anomaly at epoch: | 96.1462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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