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 67747U 26145.34254441 +.00000000 +00000-0 +27175-3 0 00004
2 67747 97.5027 273.6899 0008638 300.3879 59.6501 15.18902579 05
| Epoch (UTC): | 25 May 2026 08:13:15 |
| Eccentricity: | 0.0008638 |
| inclination: | 97.5027° |
| perigee height: | 503 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 273.6899° |
| argument of perigee: | 300.3879° |
| revolutions per day: | 15.18902579 |
| mean anomaly at epoch: | 59.6501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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