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 67919U 26145.43622727 +.00000000 +00000-0 +43602-3 0 00004
2 67919 42.9996 171.4671 0001561 273.7301 86.3372 15.27591499 07
| Epoch (UTC): | 25 May 2026 10:28:10 |
| Eccentricity: | 0.0001561 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.4671° |
| argument of perigee: | 273.7301° |
| revolutions per day: | 15.27591499 |
| mean anomaly at epoch: | 86.3372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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