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 67251U 26145.43962824 +.00000000 +00000-0 +18366-3 0 00007
2 67251 97.5692 216.7279 0149966 43.2251 318.0622 14.89534507 05
| Epoch (UTC): | 25 May 2026 10:33:03 |
| Eccentricity: | 0.0149966 |
| inclination: | 97.5692° |
| perigee height: | 495 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 216.7279° |
| argument of perigee: | 43.2251° |
| revolutions per day: | 14.89534507 |
| mean anomaly at epoch: | 318.0622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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