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 26159.34389375 +.00000000 +00000-0 +33533-3 0 00003
2 43017 97.4721 26.7398 0150896 359.9259 0.1924 15.12571253 01
| Epoch (UTC): | 08 June 2026 08:15:12 |
| Eccentricity: | 0.0150896 |
| inclination: | 97.4721° |
| perigee height: | 424 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 26.7398° |
| argument of perigee: | 359.9259° |
| revolutions per day: | 15.12571253 |
| mean anomaly at epoch: | 0.1924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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