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 20439U 26106.86163122 +.00000000 +00000-0 +44555-4 0 00002
2 20439 98.8586 141.0857 0011466 55.5884 124.7944 14.33916819 09
| Epoch (UTC): | 16 April 2026 20:40:44 |
| Eccentricity: | 0.0011466 |
| inclination: | 98.8586° |
| perigee height: | 770 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 141.0857° |
| argument of perigee: | 55.5884° |
| revolutions per day: | 14.33916819 |
| mean anomaly at epoch: | 124.7944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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