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 60406U 26145.49568598 +.00000000 +00000-0 +25629-4 0 00009
2 60406 53.1569 67.8166 0000921 87.4874 272.6249 15.69713796 07
| Epoch (UTC): | 25 May 2026 11:53:47 |
| Eccentricity: | 0.0000921 |
| inclination: | 53.1569° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 67.8166° |
| argument of perigee: | 87.4874° |
| revolutions per day: | 15.69713796 |
| mean anomaly at epoch: | 272.6249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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