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 67309U 26145.34938762 +.00000000 +00000-0 +67685-3 0 00003
2 67309 42.9979 252.2804 0000571 258.2031 101.8756 15.27593468 02
| Epoch (UTC): | 25 May 2026 08:23:07 |
| Eccentricity: | 0.0000571 |
| inclination: | 42.9979° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 252.2804° |
| argument of perigee: | 258.2031° |
| revolutions per day: | 15.27593468 |
| mean anomaly at epoch: | 101.8756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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