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 67780U 26145.50046771 +.00000000 +00000-0 +25071-3 0 00007
2 67780 51.8969 225.5202 0000876 92.2695 267.8366 14.76461724 00
| Epoch (UTC): | 25 May 2026 12:00:40 |
| Eccentricity: | 0.0000876 |
| inclination: | 51.8969° |
| perigee height: | 640 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 225.5202° |
| argument of perigee: | 92.2695° |
| revolutions per day: | 14.76461724 |
| mean anomaly at epoch: | 267.8366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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