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 68441U 26145.40958000 +.00000000 +00000-0 +19962-3 0 00000
2 68441 97.4469 104.1130 0003856 128.3138 231.8443 15.17998897 01
| Epoch (UTC): | 25 May 2026 09:49:47 |
| Eccentricity: | 0.0003856 |
| inclination: | 97.4469° |
| perigee height: | 509 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 104.1130° |
| argument of perigee: | 128.3138° |
| revolutions per day: | 15.17998897 |
| mean anomaly at epoch: | 231.8443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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