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 68917U 26161.49425235 +.00000000 +00000-0 +60665-3 0 00000
2 68917 97.2855 357.1512 0001618 101.8059 258.3365 15.33470966 09
| Epoch (UTC): | 10 June 2026 11:51:43 |
| Eccentricity: | 0.0001618 |
| inclination: | 97.2855° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 357.1512° |
| argument of perigee: | 101.8059° |
| revolutions per day: | 15.33470966 |
| mean anomaly at epoch: | 258.3365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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