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 67956U 26145.20718167 +.00000000 +00000-0 +58667-3 0 00001
2 67956 42.9991 118.5337 0001583 268.6917 91.3754 15.27586291 08
| Epoch (UTC): | 25 May 2026 04:58:20 |
| Eccentricity: | 0.0001583 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.5337° |
| argument of perigee: | 268.6917° |
| revolutions per day: | 15.27586291 |
| mean anomaly at epoch: | 91.3754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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