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 26145.57805387 +.00000000 +00000-0 +21675-3 0 00007
2 39430 97.6504 347.4673 0129440 149.5292 211.3520 14.69352981 00
| Epoch (UTC): | 25 May 2026 13:52:23 |
| Eccentricity: | 0.0129440 |
| inclination: | 97.6504° |
| perigee height: | 572 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 347.4673° |
| argument of perigee: | 149.5292° |
| revolutions per day: | 14.69352981 |
| mean anomaly at epoch: | 211.3520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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