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 68226U 26145.36916750 +.00000000 +00000-0 +41455-3 0 00004
2 68226 97.2871 20.8784 0003135 76.0857 284.0734 15.33448889 05
| Epoch (UTC): | 25 May 2026 08:51:36 |
| Eccentricity: | 0.0003135 |
| inclination: | 97.2871° |
| perigee height: | 463 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 20.8784° |
| argument of perigee: | 76.0857° |
| revolutions per day: | 15.33448889 |
| mean anomaly at epoch: | 284.0734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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