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 00005U 26140.78420384 +.00000000 +00000-0 +17045-3 0 00007
2 00005 34.2466 38.8930 1835676 14.9186 349.8894 10.85982298 05
| Epoch (UTC): | 20 May 2026 18:49:15 |
| Eccentricity: | 0.1835676 |
| inclination: | 34.2466° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 38.8930° |
| argument of perigee: | 14.9186° |
| revolutions per day: | 10.85982298 |
| mean anomaly at epoch: | 349.8894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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