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 20626U 26088.16956845 +.00000000 +00000-0 +10489-3 0 00002
2 20626 71.0191 2.9202 0208149 257.7075 261.3364 13.72948202 02
| Epoch (UTC): | 29 March 2026 04:04:10 |
| Eccentricity: | 0.0208149 |
| inclination: | 71.0191° |
| perigee height: | 836 km |
| apogee height: | 1142 km |
| right ascension of ascending node: | 2.9202° |
| argument of perigee: | 257.7075° |
| revolutions per day: | 13.72948202 |
| mean anomaly at epoch: | 261.3364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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