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 62428U 26145.26785852 +.00000000 +00000-0 +86497-3 0 00003
2 62428 42.9984 249.5306 0001611 275.6156 84.4511 15.27588997 04
| Epoch (UTC): | 25 May 2026 06:25:42 |
| Eccentricity: | 0.0001611 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 249.5306° |
| argument of perigee: | 275.6156° |
| revolutions per day: | 15.27588997 |
| mean anomaly at epoch: | 84.4511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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