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 62635U 26145.63386203 +.00000000 +00000-0 +31155-3 0 00002
2 62635 97.4002 225.8758 0003886 73.3104 286.8556 15.18965907 07
| Epoch (UTC): | 25 May 2026 15:12:45 |
| Eccentricity: | 0.0003886 |
| inclination: | 97.4002° |
| perigee height: | 506 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 225.8758° |
| argument of perigee: | 73.3104° |
| revolutions per day: | 15.18965907 |
| mean anomaly at epoch: | 286.8556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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