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 62193U 26145.47287285 +.00000000 +00000-0 +73969-3 0 00002
2 62193 43.0032 197.1529 0001913 273.8583 86.2050 15.27589595 06
| Epoch (UTC): | 25 May 2026 11:20:56 |
| Eccentricity: | 0.0001913 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.1529° |
| argument of perigee: | 273.8583° |
| revolutions per day: | 15.27589595 |
| mean anomaly at epoch: | 86.2050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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