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 62641U 26145.17425161 +.00000000 +00000-0 +38334-3 0 00001
2 62641 97.3934 226.7100 0003056 63.7769 296.3785 15.28780832 00
| Epoch (UTC): | 25 May 2026 04:10:55 |
| Eccentricity: | 0.0003056 |
| inclination: | 97.3934° |
| perigee height: | 477 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 226.7100° |
| argument of perigee: | 63.7769° |
| revolutions per day: | 15.28780832 |
| mean anomaly at epoch: | 296.3785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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