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 68020U 26145.38372459 +.00000000 +00000-0 +93194-3 0 00007
2 68020 97.2852 94.3530 0002766 102.9739 257.1813 15.33447556 07
| Epoch (UTC): | 25 May 2026 09:12:33 |
| Eccentricity: | 0.0002766 |
| inclination: | 97.2852° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3530° |
| argument of perigee: | 102.9739° |
| revolutions per day: | 15.33447556 |
| mean anomaly at epoch: | 257.1813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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