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 20438U 26106.91659822 +.00000000 +00000-0 +30337-4 0 00007
2 20438 98.7895 162.7857 0010080 164.7774 15.2089 14.31708607 08
| Epoch (UTC): | 16 April 2026 21:59:54 |
| Eccentricity: | 0.0010080 |
| inclination: | 98.7895° |
| perigee height: | 779 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 162.7857° |
| argument of perigee: | 164.7774° |
| revolutions per day: | 14.31708607 |
| mean anomaly at epoch: | 15.2089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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