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 68815U 26145.30072478 +.00000000 +00000-0 +14467-2 0 00004
2 68815 97.2856 351.9670 0001422 71.8744 288.2676 15.75255691 03
| Epoch (UTC): | 25 May 2026 07:13:02 |
| Eccentricity: | 0.0001422 |
| inclination: | 97.2856° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9670° |
| argument of perigee: | 71.8744° |
| revolutions per day: | 15.75255691 |
| mean anomaly at epoch: | 288.2676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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