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 62742U 26144.18220049 +.00000000 +00000-0 +37661-3 0 00003
2 62742 43.0015 87.9882 0001528 267.1924 92.8753 15.27586404 01
| Epoch (UTC): | 24 May 2026 04:22:22 |
| Eccentricity: | 0.0001528 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.9882° |
| argument of perigee: | 267.1924° |
| revolutions per day: | 15.27586404 |
| mean anomaly at epoch: | 92.8753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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