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 68434U 26145.39063664 +.00000000 +00000-0 +18451-3 0 00005
2 68434 97.4567 104.2400 0003420 73.0846 287.0763 15.18439599 00
| Epoch (UTC): | 25 May 2026 09:22:31 |
| Eccentricity: | 0.0003420 |
| inclination: | 97.4567° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.2400° |
| argument of perigee: | 73.0846° |
| revolutions per day: | 15.18439599 |
| mean anomaly at epoch: | 287.0763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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