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 68075U 26145.32625813 +.00000000 +00000-0 +30118-3 0 00003
2 68075 53.1587 182.4030 0001146 84.9053 275.2080 15.34397423 01
| Epoch (UTC): | 25 May 2026 07:49:48 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 182.4030° |
| argument of perigee: | 84.9053° |
| revolutions per day: | 15.34397423 |
| mean anomaly at epoch: | 275.2080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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