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 21639U 26145.51252229 +.00000000 +00000-0 +00000-0 0 00000
2 21639 14.0743 353.9520 0006577 287.2998 338.8500 1.00265922 03
| Epoch (UTC): | 25 May 2026 12:18:01 |
| Eccentricity: | 0.0006577 |
| inclination: | 14.0743° |
| perigee height: | 35761 km |
| apogee height: | 35816 km |
| right ascension of ascending node: | 353.9520° |
| argument of perigee: | 287.2998° |
| revolutions per day: | 1.00265922 |
| mean anomaly at epoch: | 338.8500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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