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 26075.96503822 +.00000000 +00000-0 +31321-3 0 00005
2 39679 51.6063 301.7801 0096870 129.5376 231.4219 15.39428092 05
| Epoch (UTC): | 16 March 2026 23:09:39 |
| Eccentricity: | 0.0096870 |
| inclination: | 51.6063° |
| perigee height: | 382 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 301.7801° |
| argument of perigee: | 129.5376° |
| revolutions per day: | 15.39428092 |
| mean anomaly at epoch: | 231.4219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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