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 68569U 26145.58335647 +.00000000 +00000-0 -84185-1 0 00004
2 68569 53.1603 4.6035 0001706 126.0601 73.3314 15.38206311 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001706 |
| inclination: | 53.1603° |
| perigee height: | 450 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 4.6035° |
| argument of perigee: | 126.0601° |
| revolutions per day: | 15.38206311 |
| mean anomaly at epoch: | 73.3314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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