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 67198U 26145.53243670 +.00000000 +00000-0 +13601-3 0 00006
2 67198 70.0018 340.7629 0002382 266.5854 93.5033 14.98333212 00
| Epoch (UTC): | 25 May 2026 12:46:42 |
| Eccentricity: | 0.0002382 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.7629° |
| argument of perigee: | 266.5854° |
| revolutions per day: | 14.98333212 |
| mean anomaly at epoch: | 93.5033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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