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 62205U 26145.57473022 +.00000000 +00000-0 +32903-3 0 00006
2 62205 43.0007 182.3160 0001979 281.3145 78.7484 15.27576426 05
| Epoch (UTC): | 25 May 2026 13:47:36 |
| Eccentricity: | 0.0001979 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.3160° |
| argument of perigee: | 281.3145° |
| revolutions per day: | 15.27576426 |
| mean anomaly at epoch: | 78.7484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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