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 68683U 26145.23215860 +.00000000 +00000-0 +49104-3 0 00000
2 68683 97.2872 16.8850 0001583 87.8635 272.2789 15.33454391 05
| Epoch (UTC): | 25 May 2026 05:34:18 |
| Eccentricity: | 0.0001583 |
| inclination: | 97.2872° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.8850° |
| argument of perigee: | 87.8635° |
| revolutions per day: | 15.33454391 |
| mean anomaly at epoch: | 272.2789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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