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 20437U 26100.40998816 +.00000000 +00000-0 +47453-4 0 00000
2 20437 98.8106 148.5221 0011507 102.1635 269.3396 14.33250826 07
| Epoch (UTC): | 10 April 2026 09:50:22 |
| Eccentricity: | 0.0011507 |
| inclination: | 98.8106° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 148.5221° |
| argument of perigee: | 102.1635° |
| revolutions per day: | 14.33250826 |
| mean anomaly at epoch: | 269.3396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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