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 62965U 26145.51822638 +.00000000 +00000-0 +66935-3 0 00006
2 62965 53.1591 233.2344 0001319 87.8882 272.2270 15.30201011 06
| Epoch (UTC): | 25 May 2026 12:26:14 |
| Eccentricity: | 0.0001319 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.2344° |
| argument of perigee: | 87.8882° |
| revolutions per day: | 15.30201011 |
| mean anomaly at epoch: | 272.2270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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