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 68886U 26145.58335647 +.00000000 +00000-0 +99618-3 0 00004
2 68886 51.8838 351.6319 0004657 192.3783 119.1634 15.34269976 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0004657 |
| inclination: | 51.8838° |
| perigee height: | 460 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 351.6319° |
| argument of perigee: | 192.3783° |
| revolutions per day: | 15.34269976 |
| mean anomaly at epoch: | 119.1634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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