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 43529U 26145.57655308 +.00000000 +00000-0 +25393-3 0 00008
2 43529 98.1247 301.1021 0021923 179.6918 180.4321 14.98955945 00
| Epoch (UTC): | 25 May 2026 13:50:14 |
| Eccentricity: | 0.0021923 |
| inclination: | 98.1247° |
| perigee height: | 555 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 301.1021° |
| argument of perigee: | 179.6918° |
| revolutions per day: | 14.98955945 |
| mean anomaly at epoch: | 180.4321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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