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 68107U 26145.38687919 +.00000000 +00000-0 +70758-3 0 00004
2 68107 97.2845 105.9587 0002251 103.0709 257.0785 15.33454947 03
| Epoch (UTC): | 25 May 2026 09:17:06 |
| Eccentricity: | 0.0002251 |
| inclination: | 97.2845° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 105.9587° |
| argument of perigee: | 103.0709° |
| revolutions per day: | 15.33454947 |
| mean anomaly at epoch: | 257.0785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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