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 26053.72003720 +.00000000 +00000-0 +38905-4 0 00006
2 20438 98.8010 108.8912 0009172 332.3978 141.4660 14.31695678 00
| Epoch (UTC): | 22 February 2026 17:16:51 |
| Eccentricity: | 0.0009172 |
| inclination: | 98.8010° |
| perigee height: | 779 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 108.8912° |
| argument of perigee: | 332.3978° |
| revolutions per day: | 14.31695678 |
| mean anomaly at epoch: | 141.4660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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