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 67562U 26145.58133676 +.00000000 +00000-0 +52528-3 0 00001
2 67562 97.2849 205.9895 0000915 313.0908 47.0258 15.33457078 03
| Epoch (UTC): | 25 May 2026 13:57:07 |
| Eccentricity: | 0.0000915 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9895° |
| argument of perigee: | 313.0908° |
| revolutions per day: | 15.33457078 |
| mean anomaly at epoch: | 47.0258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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