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 61742U 26145.61483513 +.00000000 +00000-0 +20289-3 0 00006
2 61742 97.3261 345.1251 0013481 135.2896 224.9416 14.95803073 00
| Epoch (UTC): | 25 May 2026 14:45:21 |
| Eccentricity: | 0.0013481 |
| inclination: | 97.3261° |
| perigee height: | 571 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 345.1251° |
| argument of perigee: | 135.2896° |
| revolutions per day: | 14.95803073 |
| mean anomaly at epoch: | 224.9416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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