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 26069.58859512 +.00000000 +00000-0 +54358-3 0 00002
2 43017 97.4848 298.8651 0154494 309.0184 49.7375 15.10898387 03
| Epoch (UTC): | 10 March 2026 14:07:34 |
| Eccentricity: | 0.0154494 |
| inclination: | 97.4848° |
| perigee height: | 427 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 298.8651° |
| argument of perigee: | 309.0184° |
| revolutions per day: | 15.10898387 |
| mean anomaly at epoch: | 49.7375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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