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 39428U 26106.65642916 +.00000000 +00000-0 +46387-3 0 00004
2 39428 97.8353 27.0602 0077290 52.3643 308.4558 14.94272570 02
| Epoch (UTC): | 16 April 2026 15:45:15 |
| Eccentricity: | 0.0077290 |
| inclination: | 97.8353° |
| perigee height: | 531 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 27.0602° |
| argument of perigee: | 52.3643° |
| revolutions per day: | 14.94272570 |
| mean anomaly at epoch: | 308.4558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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