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 67419U 26145.41921047 +.00000000 +00000-0 +41902-3 0 00005
2 67419 43.0000 164.4505 0001523 272.2646 87.8032 15.27586677 03
| Epoch (UTC): | 25 May 2026 10:03:39 |
| Eccentricity: | 0.0001523 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.4505° |
| argument of perigee: | 272.2646° |
| revolutions per day: | 15.27586677 |
| mean anomaly at epoch: | 87.8032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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