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 68255U 26145.40816153 +.00000000 +00000-0 +10951-2 0 00003
2 68255 53.1591 297.9925 0002042 86.3258 273.7981 15.42203501 05
| Epoch (UTC): | 25 May 2026 09:47:45 |
| Eccentricity: | 0.0002042 |
| inclination: | 53.1591° |
| perigee height: | 438 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 297.9925° |
| argument of perigee: | 86.3258° |
| revolutions per day: | 15.42203501 |
| mean anomaly at epoch: | 273.7981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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