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 68695U 26145.64152586 +.00000000 +00000-0 +33472-3 0 00004
2 68695 97.6642 221.2778 0017211 136.8187 223.4395 15.09745500 09
| Epoch (UTC): | 25 May 2026 15:23:47 |
| Eccentricity: | 0.0017211 |
| inclination: | 97.6642° |
| perigee height: | 525 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 221.2778° |
| argument of perigee: | 136.8187° |
| revolutions per day: | 15.09745500 |
| mean anomaly at epoch: | 223.4395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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