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 68594U 26145.42782628 +.00000000 +00000-0 +67982-3 0 00007
2 68594 51.8691 287.3547 0010383 304.9969 55.0042 15.36558513 03
| Epoch (UTC): | 25 May 2026 10:16:04 |
| Eccentricity: | 0.0010383 |
| inclination: | 51.8691° |
| perigee height: | 449 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 287.3547° |
| argument of perigee: | 304.9969° |
| revolutions per day: | 15.36558513 |
| mean anomaly at epoch: | 55.0042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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