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 68673U 26145.39529859 +.00000000 +00000-0 +53494-3 0 00009
2 68673 97.2847 16.9708 0001715 102.1392 258.0043 15.33442926 03
| Epoch (UTC): | 25 May 2026 09:29:13 |
| Eccentricity: | 0.0001715 |
| inclination: | 97.2847° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.9708° |
| argument of perigee: | 102.1392° |
| revolutions per day: | 15.33442926 |
| mean anomaly at epoch: | 258.0043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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