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 43923U 26145.32184824 +.00000000 +00000-0 +99260-4 0 00004
2 43923 86.6104 3.1041 0002243 87.4328 272.7146 14.72251369 09
| Epoch (UTC): | 25 May 2026 07:43:27 |
| Eccentricity: | 0.0002243 |
| inclination: | 86.6104° |
| perigee height: | 652 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 3.1041° |
| argument of perigee: | 87.4328° |
| revolutions per day: | 14.72251369 |
| mean anomaly at epoch: | 272.7146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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