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 67377U 26145.43889956 +.00000000 +00000-0 +77236-4 0 00002
2 67377 97.8033 144.4578 0002198 182.6973 177.4231 14.86245981 04
| Epoch (UTC): | 25 May 2026 10:32:00 |
| Eccentricity: | 0.0002198 |
| inclination: | 97.8033° |
| perigee height: | 608 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 144.4578° |
| argument of perigee: | 182.6973° |
| revolutions per day: | 14.86245981 |
| mean anomaly at epoch: | 177.4231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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