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 26071.57536949 +.00000000 +00000-0 +65446-3 0 00000
2 43017 97.4859 300.8129 0154357 301.9271 56.7024 15.10950627 00
| Epoch (UTC): | 12 March 2026 13:48:31 |
| Eccentricity: | 0.0154357 |
| inclination: | 97.4859° |
| perigee height: | 427 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 300.8129° |
| argument of perigee: | 301.9271° |
| revolutions per day: | 15.10950627 |
| mean anomaly at epoch: | 56.7024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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