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 39767U 26150.21802417 +.00000000 +00000-0 +36305-3 0 00004
2 39767 97.8049 247.6684 0005398 27.9664 332.1846 14.95767349 09
| Epoch (UTC): | 30 May 2026 05:13:57 |
| Eccentricity: | 0.0005398 |
| inclination: | 97.8049° |
| perigee height: | 576 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 247.6684° |
| argument of perigee: | 27.9664° |
| revolutions per day: | 14.95767349 |
| mean anomaly at epoch: | 332.1846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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