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 26110.14986102 +.00000000 +00000-0 +18734-3 0 00005
2 00005 34.2516 133.4185 1836812 236.8263 104.2767 10.85971808 06
| Epoch (UTC): | 20 April 2026 03:35:47 |
| Eccentricity: | 0.1836812 |
| inclination: | 34.2516° |
| perigee height: | 653 km |
| apogee height: | 3818 km |
| right ascension of ascending node: | 133.4185° |
| argument of perigee: | 236.8263° |
| revolutions per day: | 10.85971808 |
| mean anomaly at epoch: | 104.2767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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