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 68802U 26145.31307470 +.00000000 +00000-0 +13551-2 0 00007
2 68802 97.2851 351.9502 0001431 72.7748 287.3674 15.75245247 06
| Epoch (UTC): | 25 May 2026 07:30:49 |
| Eccentricity: | 0.0001431 |
| inclination: | 97.2851° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9502° |
| argument of perigee: | 72.7748° |
| revolutions per day: | 15.75245247 |
| mean anomaly at epoch: | 287.3674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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