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 26039.53173631 +.00000000 +00000-0 +24900-3 0 00004
2 39679 51.6065 119.4159 0099013 356.7201 3.3122 15.38245898 09
| Epoch (UTC): | 08 February 2026 12:45:42 |
| Eccentricity: | 0.0099013 |
| inclination: | 51.6065° |
| perigee height: | 384 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 119.4159° |
| argument of perigee: | 356.7201° |
| revolutions per day: | 15.38245898 |
| mean anomaly at epoch: | 3.3122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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