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 62212U 26145.48492269 +.00000000 +00000-0 +33517-3 0 00000
2 62212 42.9995 193.7797 0001513 276.1709 83.8970 15.27588020 01
| Epoch (UTC): | 25 May 2026 11:38:17 |
| Eccentricity: | 0.0001513 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.7797° |
| argument of perigee: | 276.1709° |
| revolutions per day: | 15.27588020 |
| mean anomaly at epoch: | 83.8970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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