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 67795U 26145.54910716 +.00000000 +00000-0 +41948-3 0 00007
2 67795 51.8794 208.4818 0007787 328.9526 31.0999 15.35508838 02
| Epoch (UTC): | 25 May 2026 13:10:42 |
| Eccentricity: | 0.0007787 |
| inclination: | 51.8794° |
| perigee height: | 454 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 208.4818° |
| argument of perigee: | 328.9526° |
| revolutions per day: | 15.35508838 |
| mean anomaly at epoch: | 31.0999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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