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 39417U 26138.14345683 +.00000000 +00000-0 +24772-3 0 00006
2 39417 97.8123 100.3176 0041199 353.8882 6.1833 15.00938209 03
| Epoch (UTC): | 18 May 2026 03:26:34 |
| Eccentricity: | 0.0041199 |
| inclination: | 97.8123° |
| perigee height: | 535 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 100.3176° |
| argument of perigee: | 353.8882° |
| revolutions per day: | 15.00938209 |
| mean anomaly at epoch: | 6.1833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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