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 43930U 26145.53192543 +.00000000 +00000-0 +95811-4 0 00000
2 43930 86.6104 3.0189 0002383 90.0405 270.1086 14.72254397 09
| Epoch (UTC): | 25 May 2026 12:45:58 |
| Eccentricity: | 0.0002383 |
| inclination: | 86.6104° |
| perigee height: | 652 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 3.0189° |
| argument of perigee: | 90.0405° |
| revolutions per day: | 14.72254397 |
| mean anomaly at epoch: | 270.1086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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