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 68359U 26145.36151875 +.00000000 +00000-0 +18535-3 0 00003
2 68359 54.9766 128.9872 0014067 98.1763 262.0831 14.73360464 09
| Epoch (UTC): | 25 May 2026 08:40:35 |
| Eccentricity: | 0.0014067 |
| inclination: | 54.9766° |
| perigee height: | 640 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 128.9872° |
| argument of perigee: | 98.1763° |
| revolutions per day: | 14.73360464 |
| mean anomaly at epoch: | 262.0831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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