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 68686U 26145.62912840 +.00000000 +00000-0 +27104-3 0 00004
2 68686 97.2859 17.2633 0001645 122.3112 237.8290 15.33455006 09
| Epoch (UTC): | 25 May 2026 15:05:56 |
| Eccentricity: | 0.0001645 |
| inclination: | 97.2859° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.2633° |
| argument of perigee: | 122.3112° |
| revolutions per day: | 15.33455006 |
| mean anomaly at epoch: | 237.8290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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