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 43017U 26073.62831316 +.00000000 +00000-0 +61706-3 0 00009
2 43017 97.4861 302.8209 0153791 295.0415 63.4915 15.10996825 02
| Epoch (UTC): | 14 March 2026 15:04:46 |
| Eccentricity: | 0.0153791 |
| inclination: | 97.4861° |
| perigee height: | 427 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 302.8209° |
| argument of perigee: | 295.0415° |
| revolutions per day: | 15.10996825 |
| mean anomaly at epoch: | 63.4915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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