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 67050U 26145.20312117 +.00000000 +00000-0 +46150-3 0 00005
2 67050 43.0045 325.7286 0000561 263.1997 96.8791 15.27582912 00
| Epoch (UTC): | 25 May 2026 04:52:29 |
| Eccentricity: | 0.0000561 |
| inclination: | 43.0045° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 325.7286° |
| argument of perigee: | 263.1997° |
| revolutions per day: | 15.27582912 |
| mean anomaly at epoch: | 96.8791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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