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 57355U 26145.50861351 +.00000000 +00000-0 -32071-5 0 00004
2 57355 43.0024 168.2014 0001434 285.2866 74.7827 15.27578340 08
| Epoch (UTC): | 25 May 2026 12:12:24 |
| Eccentricity: | 0.0001434 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.2014° |
| argument of perigee: | 285.2866° |
| revolutions per day: | 15.27578340 |
| mean anomaly at epoch: | 74.7827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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