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 60439U 26145.58602847 +.00000000 +00000-0 -32390-4 0 00005
2 60439 53.1604 219.1531 0001306 86.5989 273.5163 15.34375820 05
| Epoch (UTC): | 25 May 2026 14:03:52 |
| Eccentricity: | 0.0001306 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 219.1531° |
| argument of perigee: | 86.5989° |
| revolutions per day: | 15.34375820 |
| mean anomaly at epoch: | 273.5163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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