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 67909U 26145.54144983 +.00000000 +00000-0 +54671-3 0 00006
2 67909 43.0015 171.4186 0001859 270.5713 89.4925 15.27591436 02
| Epoch (UTC): | 25 May 2026 12:59:41 |
| Eccentricity: | 0.0001859 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.4186° |
| argument of perigee: | 270.5713° |
| revolutions per day: | 15.27591436 |
| mean anomaly at epoch: | 89.4925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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