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 60425U 26145.48819227 +.00000000 +00000-0 +16550-4 0 00000
2 60425 53.1591 220.6763 0000898 67.0930 293.0165 15.30189554 06
| Epoch (UTC): | 25 May 2026 11:42:59 |
| Eccentricity: | 0.0000898 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.6763° |
| argument of perigee: | 67.0930° |
| revolutions per day: | 15.30189554 |
| mean anomaly at epoch: | 293.0165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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