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 61751U 26145.62351201 +.00000000 +00000-0 +24782-3 0 00007
2 61751 97.3033 15.2459 0010683 37.7547 322.4444 15.36371906 08
| Epoch (UTC): | 25 May 2026 14:57:51 |
| Eccentricity: | 0.0010683 |
| inclination: | 97.3033° |
| perigee height: | 450 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 15.2459° |
| argument of perigee: | 37.7547° |
| revolutions per day: | 15.36371906 |
| mean anomaly at epoch: | 322.4444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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