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 67679U 26145.46361972 +.00000000 +00000-0 +44470-3 0 00006
2 67679 96.6238 212.0488 0019513 203.0866 156.9499 15.24885376 02
| Epoch (UTC): | 25 May 2026 11:07:36 |
| Eccentricity: | 0.0019513 |
| inclination: | 96.6238° |
| perigee height: | 478 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 212.0488° |
| argument of perigee: | 203.0866° |
| revolutions per day: | 15.24885376 |
| mean anomaly at epoch: | 156.9499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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