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 26155.11605369 +.00000000 +00000-0 +50981-4 0 00007
2 20438 98.7844 211.5753 0010352 35.4918 31.3710 14.31718359 01
| Epoch (UTC): | 04 June 2026 02:47:07 |
| Eccentricity: | 0.0010352 |
| inclination: | 98.7844° |
| perigee height: | 779 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 211.5753° |
| argument of perigee: | 35.4918° |
| revolutions per day: | 14.31718359 |
| mean anomaly at epoch: | 31.3710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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