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 43575U 26145.53780668 +.00000000 +00000-0 +80085-5 0 00004
2 43575 86.3967 66.1907 0002369 85.5241 274.6225 14.34217931 02
| Epoch (UTC): | 25 May 2026 12:54:26 |
| Eccentricity: | 0.0002369 |
| inclination: | 86.3967° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.1907° |
| argument of perigee: | 85.5241° |
| revolutions per day: | 14.34217931 |
| mean anomaly at epoch: | 274.6225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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