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 68876U 26145.60028632 +.00000000 +00000-0 +10446-2 0 00000
2 68876 51.8777 351.6493 0006360 204.3490 155.7197 15.37458315 07
| Epoch (UTC): | 25 May 2026 14:24:24 |
| Eccentricity: | 0.0006360 |
| inclination: | 51.8777° |
| perigee height: | 449 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 351.6493° |
| argument of perigee: | 204.3490° |
| revolutions per day: | 15.37458315 |
| mean anomaly at epoch: | 155.7197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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