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 39679U 26020.23289137 +.00000000 +00000-0 +36387-3 0 00002
2 39679 51.6052 213.3878 0099168 286.0879 72.9204 15.37629720 06
| Epoch (UTC): | 20 January 2026 05:35:21 |
| Eccentricity: | 0.0099168 |
| inclination: | 51.6052° |
| perigee height: | 385 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 213.3878° |
| argument of perigee: | 286.0879° |
| revolutions per day: | 15.37629720 |
| mean anomaly at epoch: | 72.9204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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