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 57813U 26145.49147507 +.00000000 +00000-0 +28550-4 0 00006
2 57813 43.0062 160.4937 0002041 268.4919 91.5699 15.27576524 00
| Epoch (UTC): | 25 May 2026 11:47:43 |
| Eccentricity: | 0.0002041 |
| inclination: | 43.0062° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.4937° |
| argument of perigee: | 268.4919° |
| revolutions per day: | 15.27576524 |
| mean anomaly at epoch: | 91.5699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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