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 39430U 26075.29515970 +.00000000 +00000-0 +28178-3 0 00009
2 39430 97.6568 281.5883 0129787 16.4137 344.1212 14.69125465 03
| Epoch (UTC): | 16 March 2026 07:05:01 |
| Eccentricity: | 0.0129787 |
| inclination: | 97.6568° |
| perigee height: | 572 km |
| apogee height: | 755 km |
| right ascension of ascending node: | 281.5883° |
| argument of perigee: | 16.4137° |
| revolutions per day: | 14.69125465 |
| mean anomaly at epoch: | 344.1212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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