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 67850U 26145.45803465 +.00000000 +00000-0 +77234-3 0 00008
2 67850 53.1573 207.3747 0000731 72.5775 287.5306 15.30197734 07
| Epoch (UTC): | 25 May 2026 10:59:34 |
| Eccentricity: | 0.0000731 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.3747° |
| argument of perigee: | 72.5775° |
| revolutions per day: | 15.30197734 |
| mean anomaly at epoch: | 287.5306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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