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 60942U 26145.39853141 +.00000000 +00000-0 +40256-2 0 00005
2 60942 53.1591 133.4849 0000748 119.3842 240.7234 15.31149765 00
| Epoch (UTC): | 25 May 2026 09:33:53 |
| Eccentricity: | 0.0000748 |
| inclination: | 53.1591° |
| perigee height: | 472 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 133.4849° |
| argument of perigee: | 119.3842° |
| revolutions per day: | 15.31149765 |
| mean anomaly at epoch: | 240.7234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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