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 43016U 26145.57540126 +.00000000 +00000-0 +65044-3 0 00007
2 43016 97.4664 27.9306 0109084 354.6160 5.3898 15.31057034 08
| Epoch (UTC): | 25 May 2026 13:48:34 |
| Eccentricity: | 0.0109084 |
| inclination: | 97.4664° |
| perigee height: | 398 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 27.9306° |
| argument of perigee: | 354.6160° |
| revolutions per day: | 15.31057034 |
| mean anomaly at epoch: | 5.3898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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