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 61961U 26145.26846221 +.00000000 +00000-0 +51236-3 0 00005
2 61961 43.0029 100.2600 0001591 270.6735 89.3935 15.27572969 08
| Epoch (UTC): | 25 May 2026 06:26:35 |
| Eccentricity: | 0.0001591 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2600° |
| argument of perigee: | 270.6735° |
| revolutions per day: | 15.27572969 |
| mean anomaly at epoch: | 89.3935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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