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 60531U 26145.16699758 +.00000000 +00000-0 +24896-3 0 00009
2 60531 97.6839 221.7631 0002945 85.9605 274.1954 14.98667501 03
| Epoch (UTC): | 25 May 2026 04:00:28 |
| Eccentricity: | 0.0002945 |
| inclination: | 97.6839° |
| perigee height: | 569 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 221.7631° |
| argument of perigee: | 85.9605° |
| revolutions per day: | 14.98667501 |
| mean anomaly at epoch: | 274.1954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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