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 67629U 26145.49941029 +.00000000 +00000-0 +74551-3 0 00004
2 67629 43.0073 65.7349 0002031 263.6611 96.4009 15.27587037 07
| Epoch (UTC): | 25 May 2026 11:59:09 |
| Eccentricity: | 0.0002031 |
| inclination: | 43.0073° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.7349° |
| argument of perigee: | 263.6611° |
| revolutions per day: | 15.27587037 |
| mean anomaly at epoch: | 96.4009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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