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 57356U 26145.49961753 +.00000000 +00000-0 +39996-4 0 00001
2 57356 43.0002 168.1321 0001112 275.2591 84.8133 15.27581842 05
| Epoch (UTC): | 25 May 2026 11:59:26 |
| Eccentricity: | 0.0001112 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.1321° |
| argument of perigee: | 275.2591° |
| revolutions per day: | 15.27581842 |
| mean anomaly at epoch: | 84.8133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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