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 62210U 26145.45746867 +.00000000 +00000-0 +46341-3 0 00000
2 62210 43.0070 197.0297 0000722 277.9266 82.1504 15.27564480 04
| Epoch (UTC): | 25 May 2026 10:58:45 |
| Eccentricity: | 0.0000722 |
| inclination: | 43.0070° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.0297° |
| argument of perigee: | 277.9266° |
| revolutions per day: | 15.27564480 |
| mean anomaly at epoch: | 82.1504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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