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 62206U 26145.44331808 +.00000000 +00000-0 +34526-3 0 00001
2 62206 43.0002 196.9242 0001369 272.9731 87.0964 15.27586187 04
| Epoch (UTC): | 25 May 2026 10:38:22 |
| Eccentricity: | 0.0001369 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.9242° |
| argument of perigee: | 272.9731° |
| revolutions per day: | 15.27586187 |
| mean anomaly at epoch: | 87.0964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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