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 61743U 26145.61646476 +.00000000 +00000-0 +20166-3 0 00000
2 61743 97.3241 346.5459 0007150 136.1294 224.0498 14.97737695 01
| Epoch (UTC): | 25 May 2026 14:47:42 |
| Eccentricity: | 0.0007150 |
| inclination: | 97.3241° |
| perigee height: | 569 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 346.5459° |
| argument of perigee: | 136.1294° |
| revolutions per day: | 14.97737695 |
| mean anomaly at epoch: | 224.0498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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