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 62194U 26145.57794264 +.00000000 +00000-0 +77248-3 0 00008
2 62194 43.0013 196.2162 0001341 275.5238 84.5461 15.27593637 09
| Epoch (UTC): | 25 May 2026 13:52:14 |
| Eccentricity: | 0.0001341 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.2162° |
| argument of perigee: | 275.5238° |
| revolutions per day: | 15.27593637 |
| mean anomaly at epoch: | 84.5461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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