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 67981U 26145.49424433 +.00000000 +00000-0 +61073-3 0 00005
2 67981 97.2842 155.5769 0000759 23.9966 336.1312 15.33456119 06
| Epoch (UTC): | 25 May 2026 11:51:42 |
| Eccentricity: | 0.0000759 |
| inclination: | 97.2842° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.5769° |
| argument of perigee: | 23.9966° |
| revolutions per day: | 15.33456119 |
| mean anomaly at epoch: | 336.1312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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