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 67950U 26145.63291372 +.00000000 +00000-0 +53507-3 0 00004
2 67950 42.9984 116.5938 0000647 273.4470 86.6307 15.27581377 08
| Epoch (UTC): | 25 May 2026 15:11:23 |
| Eccentricity: | 0.0000647 |
| inclination: | 42.9984° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 116.5938° |
| argument of perigee: | 273.4470° |
| revolutions per day: | 15.27581377 |
| mean anomaly at epoch: | 86.6307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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