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 68392U 26145.36021163 +.00000000 +00000-0 +52067-3 0 00004
2 68392 97.2845 287.8935 0001117 38.3203 321.8119 15.33458257 04
| Epoch (UTC): | 25 May 2026 08:38:42 |
| Eccentricity: | 0.0001117 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.8935° |
| argument of perigee: | 38.3203° |
| revolutions per day: | 15.33458257 |
| mean anomaly at epoch: | 321.8119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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