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 68545U 26145.58335647 +.00000000 +00000-0 +17970-2 0 00006
2 68545 53.1605 5.1888 0001261 93.8717 167.0936 15.34372483 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001261 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 5.1888° |
| argument of perigee: | 93.8717° |
| revolutions per day: | 15.34372483 |
| mean anomaly at epoch: | 167.0936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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