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 57733U 26145.61863562 +.00000000 +00000-0 +56755-4 0 00005
2 57733 43.0061 105.4968 0001879 285.6591 74.4053 15.26747891 08
| Epoch (UTC): | 25 May 2026 14:50:50 |
| Eccentricity: | 0.0001879 |
| inclination: | 43.0061° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 105.4968° |
| argument of perigee: | 285.6591° |
| revolutions per day: | 15.26747891 |
| mean anomaly at epoch: | 74.4053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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