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 67750U 26145.32128492 +.00000000 +00000-0 +28696-3 0 00001
2 67750 97.5042 273.7414 0008167 310.5042 49.5480 15.19234798 08
| Epoch (UTC): | 25 May 2026 07:42:39 |
| Eccentricity: | 0.0008167 |
| inclination: | 97.5042° |
| perigee height: | 503 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 273.7414° |
| argument of perigee: | 310.5042° |
| revolutions per day: | 15.19234798 |
| mean anomaly at epoch: | 49.5480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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