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 68767U 26145.58335647 +.00000000 +00000-0 -21477-1 0 00009
2 68767 97.2845 182.4384 0001589 71.2377 66.0733 15.64722039 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001589 |
| inclination: | 97.2845° |
| perigee height: | 373 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 182.4384° |
| argument of perigee: | 71.2377° |
| revolutions per day: | 15.64722039 |
| mean anomaly at epoch: | 66.0733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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