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 61740U 26145.62705385 +.00000000 +00000-0 +24895-3 0 00006
2 61740 97.3262 345.1078 0013895 133.8679 226.3694 14.95777561 04
| Epoch (UTC): | 25 May 2026 15:02:57 |
| Eccentricity: | 0.0013895 |
| inclination: | 97.3262° |
| perigee height: | 570 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 345.1078° |
| argument of perigee: | 133.8679° |
| revolutions per day: | 14.95777561 |
| mean anomaly at epoch: | 226.3694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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