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 56963U 26145.66289228 +.00000000 +00000-0 +54786-3 0 00006
2 56963 97.5857 290.3934 0002580 39.3591 320.7852 15.58285954 06
| Epoch (UTC): | 25 May 2026 15:54:33 |
| Eccentricity: | 0.0002580 |
| inclination: | 97.5857° |
| perigee height: | 391 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 290.3934° |
| argument of perigee: | 39.3591° |
| revolutions per day: | 15.58285954 |
| mean anomaly at epoch: | 320.7852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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