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 57333U 26145.49818222 +.00000000 +00000-0 +32172-4 0 00007
2 57333 43.0021 178.5992 0001501 273.1399 86.9281 15.27576850 05
| Epoch (UTC): | 25 May 2026 11:57:22 |
| Eccentricity: | 0.0001501 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.5992° |
| argument of perigee: | 273.1399° |
| revolutions per day: | 15.27576850 |
| mean anomaly at epoch: | 86.9281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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