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 68574U 26145.38682586 +.00000000 +00000-0 +36824-3 0 00003
2 68574 51.8989 298.5129 0000804 231.0610 129.0279 14.76322404 06
| Epoch (UTC): | 25 May 2026 09:17:01 |
| Eccentricity: | 0.0000804 |
| inclination: | 51.8989° |
| perigee height: | 640 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 298.5129° |
| argument of perigee: | 231.0610° |
| revolutions per day: | 14.76322404 |
| mean anomaly at epoch: | 129.0279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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