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 26101.37114122 +.00000000 +00000-0 +32900-3 0 00006
2 43017 97.4811 329.9828 0153186 198.5881 160.9718 15.11557141 05
| Epoch (UTC): | 11 April 2026 08:54:26 |
| Eccentricity: | 0.0153186 |
| inclination: | 97.4811° |
| perigee height: | 426 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 329.9828° |
| argument of perigee: | 198.5881° |
| revolutions per day: | 15.11557141 |
| mean anomaly at epoch: | 160.9718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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