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 62561U 26145.10951894 +.00000000 +00000-0 +12286-2 0 00009
2 62561 43.0041 39.0444 0002658 256.5448 103.5123 15.70893966 02
| Epoch (UTC): | 25 May 2026 02:37:42 |
| Eccentricity: | 0.0002658 |
| inclination: | 43.0041° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 39.0444° |
| argument of perigee: | 256.5448° |
| revolutions per day: | 15.70893966 |
| mean anomaly at epoch: | 103.5123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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