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 67197U 26145.50321637 +.00000000 +00000-0 +25108-3 0 00007
2 67197 70.0020 340.6589 0002297 270.4248 89.6648 14.98337819 07
| Epoch (UTC): | 25 May 2026 12:04:37 |
| Eccentricity: | 0.0002297 |
| inclination: | 70.0020° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.6589° |
| argument of perigee: | 270.4248° |
| revolutions per day: | 14.98337819 |
| mean anomaly at epoch: | 89.6648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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