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 39343U 26106.31146794 +.00000000 +00000-0 -18703-3 0 00008
2 39343 21.8226 48.3250 7120388 186.4795 153.3436 2.32933399 04
| Epoch (UTC): | 16 April 2026 07:28:30 |
| Eccentricity: | 0.7120388 |
| inclination: | 21.8226° |
| perigee height: | 544 km |
| apogee height: | 34777 km |
| right ascension of ascending node: | 48.3250° |
| argument of perigee: | 186.4795° |
| revolutions per day: | 2.32933399 |
| mean anomaly at epoch: | 153.3436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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