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 68123U 26145.33249667 +.00000000 +00000-0 +82463-3 0 00007
2 68123 97.2855 106.0340 0001087 113.0929 247.0428 15.33461280 03
| Epoch (UTC): | 25 May 2026 07:58:47 |
| Eccentricity: | 0.0001087 |
| inclination: | 97.2855° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.0340° |
| argument of perigee: | 113.0929° |
| revolutions per day: | 15.33461280 |
| mean anomaly at epoch: | 247.0428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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