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 20629U 26088.07187066 +.00000000 +00000-0 +11101-3 0 00008
2 20629 71.0231 318.9943 0198765 179.1140 343.9511 13.74146087 08
| Epoch (UTC): | 29 March 2026 01:43:29 |
| Eccentricity: | 0.0198765 |
| inclination: | 71.0231° |
| perigee height: | 838 km |
| apogee height: | 1131 km |
| right ascension of ascending node: | 318.9943° |
| argument of perigee: | 179.1140° |
| revolutions per day: | 13.74146087 |
| mean anomaly at epoch: | 343.9511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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