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 26071.68541463 +.00000000 +00000-0 +35248-3 0 00000
2 39430 97.6569 278.2039 0130071 27.9580 332.8535 14.69112124 07
| Epoch (UTC): | 12 March 2026 16:26:59 |
| Eccentricity: | 0.0130071 |
| inclination: | 97.6569° |
| perigee height: | 572 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 278.2039° |
| argument of perigee: | 27.9580° |
| revolutions per day: | 14.69112124 |
| mean anomaly at epoch: | 332.8535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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