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 62221U 26145.25938722 +.00000000 +00000-0 +14986-2 0 00002
2 62221 53.1568 84.0980 0001042 132.6523 227.4583 15.69787947 05
| Epoch (UTC): | 25 May 2026 06:13:31 |
| Eccentricity: | 0.0001042 |
| inclination: | 53.1568° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 84.0980° |
| argument of perigee: | 132.6523° |
| revolutions per day: | 15.69787947 |
| mean anomaly at epoch: | 227.4583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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