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 68916U 26145.58335647 +.00000000 +00000-0 -57577-1 0 00005
2 68916 97.2846 341.4641 0001572 85.2871 295.4790 15.42180865 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001572 |
| inclination: | 97.2846° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 341.4641° |
| argument of perigee: | 85.2871° |
| revolutions per day: | 15.42180865 |
| mean anomaly at epoch: | 295.4790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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