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 68344U 26145.01341102 +.00000000 +00000-0 +45382-3 0 00003
2 68344 53.1578 354.2882 0001193 89.6301 270.4837 15.29375776 02
| Epoch (UTC): | 25 May 2026 00:19:18 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.1578° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 354.2882° |
| argument of perigee: | 89.6301° |
| revolutions per day: | 15.29375776 |
| mean anomaly at epoch: | 270.4837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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