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 68731U 26145.58335647 +.00000000 +00000-0 -41609-1 0 00009
2 68731 97.2854 9.2324 0001700 98.4852 226.3833 15.54458512 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001700 |
| inclination: | 97.2854° |
| perigee height: | 403 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 9.2324° |
| argument of perigee: | 98.4852° |
| revolutions per day: | 15.54458512 |
| mean anomaly at epoch: | 226.3833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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