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 20798U 26100.21084431 +.00000000 +00000-0 +42119-3 0 00001
2 20798 98.7680 88.9002 0009203 138.1473 222.0410 14.22049997 02
| Epoch (UTC): | 10 April 2026 05:03:36 |
| Eccentricity: | 0.0009203 |
| inclination: | 98.7680° |
| perigee height: | 812 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 88.9002° |
| argument of perigee: | 138.1473° |
| revolutions per day: | 14.22049997 |
| mean anomaly at epoch: | 222.0410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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