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 68975U 26145.58335647 +.00000000 +00000-0 -29510-1 0 00006
2 68975 53.1592 267.9527 0001228 62.4456 98.0962 15.60525318 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.1592° |
| perigee height: | 385 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 267.9527° |
| argument of perigee: | 62.4456° |
| revolutions per day: | 15.60525318 |
| mean anomaly at epoch: | 98.0962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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