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 26071.17802108 +.00000000 +00000-0 +46531-3 0 00003
2 43017 97.4859 300.4219 0154325 303.5075 55.1489 15.10934908 03
| Epoch (UTC): | 12 March 2026 04:16:21 |
| Eccentricity: | 0.0154325 |
| inclination: | 97.4859° |
| perigee height: | 427 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 300.4219° |
| argument of perigee: | 303.5075° |
| revolutions per day: | 15.10934908 |
| mean anomaly at epoch: | 55.1489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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