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 39216U 26107.89216601 +.00000000 +00000-0 +00000-0 0 00003
2 39216 1.7699 83.2662 0001300 255.3730 318.0589 1.00268964 01
| Epoch (UTC): | 17 April 2026 21:24:43 |
| Eccentricity: | 0.0001300 |
| inclination: | 1.7699° |
| perigee height: | 35782 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 83.2662° |
| argument of perigee: | 255.3730° |
| revolutions per day: | 1.00268964 |
| mean anomaly at epoch: | 318.0589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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