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 61739U 26145.58602681 +.00000000 +00000-0 +18306-3 0 00004
2 61739 97.3274 344.8619 0013739 133.8493 226.3866 14.95016874 07
| Epoch (UTC): | 25 May 2026 14:03:52 |
| Eccentricity: | 0.0013739 |
| inclination: | 97.3274° |
| perigee height: | 573 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 344.8619° |
| argument of perigee: | 133.8493° |
| revolutions per day: | 14.95016874 |
| mean anomaly at epoch: | 226.3866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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